mirror of
https://github.com/ArthurIdema/Zoekeend-Phrase-Indexing.git
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44 KiB
44 KiB
| 1 | 1 | vice versa | 2 |
|---|---|---|---|
| 2 | 2 | ammonium chloride | 1 |
| 3 | 3 | inorganic salts | 2 |
| 4 | 4 | international geophysical | 1 |
| 5 | 5 | dislocation climb | 1 |
| 6 | 6 | slipstreams downward | 1 |
| 7 | 8 | lagrangian multiplier | 2 |
| 8 | 10 | spark schlieren | 1 |
| 9 | 12 | generalised airforces | 1 |
| 10 | 13 | solar activity | 2 |
| 11 | 14 | retrocket exhausting | 1 |
| 12 | 15 | current status | 3 |
| 13 | 16 | flame stabilization | 2 |
| 14 | 17 | apparently unlimited | 2 |
| 15 | 18 | cambered ogee | 1 |
| 16 | 19 | thermo mechanical | 2 |
| 17 | 21 | sea level | 2 |
| 18 | 22 | chapman rubesin | 2 |
| 19 | 23 | effective tripping | 2 |
| 20 | 24 | feeding sheet | 1 |
| 21 | 26 | extendible afterbody | 1 |
| 22 | 27 | practically unaffected | 2 |
| 23 | 28 | disk spring | 2 |
| 24 | 29 | semiempirical lifetime | 1 |
| 25 | 30 | multiplicative factor | 2 |
| 26 | 32 | dual rotating | 2 |
| 27 | 33 | magnetohydrodynamics shocks | 1 |
| 28 | 34 | reciprocity relations | 1 |
| 29 | 36 | midplane compressive | 2 |
| 30 | 37 | initially imperfect | 2 |
| 31 | 38 | inflection points | 2 |
| 32 | 39 | unique relationship | 2 |
| 33 | 40 | tentative conclusions | 2 |
| 34 | 41 | mathematical tools | 2 |
| 35 | 42 | short periods | 2 |
| 36 | 43 | housing sonic | 1 |
| 37 | 45 | rhombic cross | 2 |
| 38 | 46 | martian atmosphere | 2 |
| 39 | 47 | aeronautical laboratory | 2 |
| 40 | 49 | manned space | 1 |
| 41 | 50 | middle stages | 2 |
| 42 | 51 | conceptual approach | 1 |
| 43 | 52 | neutral particle | 2 |
| 44 | 53 | opposite sides | 2 |
| 45 | 54 | blunted glider | 1 |
| 46 | 55 | circulation strengths | 1 |
| 47 | 56 | diurnal variations | 1 |
| 48 | 57 | seventh power | 2 |
| 49 | 58 | localized mass | 3 |
| 50 | 59 | curve slope | 8 |
| 51 | 61 | curved aluminium | 1 |
| 52 | 62 | payload shapes | 1 |
| 53 | 63 | slight modification | 3 |
| 54 | 64 | rotating isothermal | 1 |
| 55 | 66 | rotary derivatives | 2 |
| 56 | 68 | physical interpretation | 3 |
| 57 | 69 | torsional oscillation | 2 |
| 58 | 70 | kernel function | 4 |
| 59 | 71 | agrees closely | 2 |
| 60 | 72 | electric current | 2 |
| 61 | 73 | mathieu functions | 2 |
| 62 | 74 | half conic | 1 |
| 63 | 75 | fit curves | 2 |
| 64 | 76 | national physical | 2 |
| 65 | 77 | external stores | 2 |
| 66 | 78 | gravity locations | 1 |
| 67 | 79 | tapered sweptback | 1 |
| 68 | 80 | momentary stability | 1 |
| 69 | 81 | proposed programme | 1 |
| 70 | 82 | impeller blades | 1 |
| 71 | 83 | stanton tube | 1 |
| 72 | 85 | wind tunnels | 20 |
| 73 | 86 | fixed ends | 1 |
| 74 | 87 | upstream transpiration | 1 |
| 75 | 88 | chord aft | 1 |
| 76 | 89 | isolated points | 2 |
| 77 | 90 | hypervelocity vehicles | 1 |
| 78 | 91 | stiffened web | 1 |
| 79 | 92 | upper bound | 1 |
| 80 | 93 | thrust hypothesis | 1 |
| 81 | 94 | highly swept | 4 |
| 82 | 95 | principal features | 1 |
| 83 | 96 | quasi steady | 8 |
| 84 | 98 | load carrying | 2 |
| 85 | 99 | shearing stress | 5 |
| 86 | 100 | working sections | 1 |
| 87 | 101 | intermediate regime | 1 |
| 88 | 102 | iteration process | 1 |
| 89 | 103 | roughness element | 3 |
| 90 | 104 | numerically integrated | 2 |
| 91 | 105 | truncated cones | 1 |
| 92 | 106 | pitot static | 5 |
| 93 | 107 | electromagnetic waves | 1 |
| 94 | 108 | flap chord | 1 |
| 95 | 110 | magnetohydrodynamic channel | 1 |
| 96 | 111 | impeller tip | 1 |
| 97 | 112 | fluid mechanics | 4 |
| 98 | 114 | semiempirical approach | 1 |
| 99 | 115 | fatigue behaviour | 3 |
| 100 | 116 | cylindrical shells | 35 |
| 101 | 117 | large flares | 1 |
| 102 | 118 | physical laboratory | 1 |
| 103 | 119 | distributed roughness | 4 |
| 104 | 120 | power spectra | 2 |
| 105 | 121 | hemisphere cylinder | 13 |
| 106 | 122 | straight line | 5 |
| 107 | 123 | gravity position | 2 |
| 108 | 124 | presented graphically | 2 |
| 109 | 125 | net mass | 2 |
| 110 | 126 | emitted thermal | 1 |
| 111 | 127 | molecular vibrations | 1 |
| 112 | 128 | oseen approximation | 2 |
| 113 | 129 | atmospheric density | 7 |
| 114 | 130 | membrane approach | 1 |
| 115 | 131 | nose bluntness | 8 |
| 116 | 132 | shroud profiles | 1 |
| 117 | 133 | limiting cases | 7 |
| 118 | 134 | instantaneous energy | 1 |
| 119 | 135 | suction quantities | 1 |
| 120 | 136 | walled circular | 1 |
| 121 | 137 | elliptic cones | 2 |
| 122 | 138 | creep collapse | 2 |
| 123 | 139 | vertical gust | 3 |
| 124 | 141 | gas rarefaction | 1 |
| 125 | 142 | held constant | 4 |
| 126 | 143 | isentropic sound | 2 |
| 127 | 144 | aileron deflections | 1 |
| 128 | 145 | discussed concerns | 1 |
| 129 | 146 | internal liquid | 1 |
| 130 | 147 | turbulent lubrication | 1 |
| 131 | 148 | arbitrary hub | 2 |
| 132 | 149 | cross coupling | 2 |
| 133 | 150 | tentative design | 1 |
| 134 | 151 | sandwich type | 4 |
| 135 | 152 | axisymmetric deformations | 1 |
| 136 | 154 | quantitative comparison | 2 |
| 137 | 155 | present writer | 2 |
| 138 | 156 | mechanical loading | 1 |
| 139 | 157 | axisymmetrical laminar | 1 |
| 140 | 158 | strong bow | 2 |
| 141 | 159 | jeffrey hamel | 1 |
| 142 | 161 | vapour screen | 1 |
| 143 | 162 | reviewer believes | 3 |
| 144 | 163 | throttle holes | 1 |
| 145 | 164 | open ended | 2 |
| 146 | 165 | fourier transforms | 3 |
| 147 | 166 | auxiliary slot | 1 |
| 148 | 167 | multiple valued | 2 |
| 149 | 169 | rayleigh ritz | 5 |
| 150 | 170 | perforated strips | 1 |
| 151 | 171 | vessel heads | 1 |
| 152 | 173 | asymptotically approaches | 1 |
| 153 | 174 | reaction resisted | 1 |
| 154 | 175 | instabilities arising | 1 |
| 155 | 176 | vibration isolation | 1 |
| 156 | 177 | minor axes | 1 |
| 157 | 178 | electrically conducting | 19 |
| 158 | 179 | finned missile | 1 |
| 159 | 180 | arbitrarily shaped | 2 |
| 160 | 181 | manoeuvring technique | 1 |
| 161 | 182 | choke line | 1 |
| 162 | 183 | axisymmetric snap | 1 |
| 163 | 185 | pivotal points | 2 |
| 164 | 186 | swept back | 7 |
| 165 | 187 | chemical kinetics | 2 |
| 166 | 189 | twin propeller | 1 |
| 167 | 193 | activation energy | 1 |
| 168 | 194 | cross sectional | 14 |
| 169 | 195 | roughness bands | 2 |
| 170 | 197 | charged satellite | 2 |
| 171 | 198 | vibrational degrees | 1 |
| 172 | 199 | series cowlings | 1 |
| 173 | 200 | power plant | 2 |
| 174 | 201 | longitudinally varying | 1 |
| 175 | 202 | dissociation scaling | 1 |
| 176 | 203 | double fourier | 2 |
| 177 | 204 | reciprocal relations | 2 |
| 178 | 206 | vibrational relaxation | 2 |
| 179 | 208 | initial eccentricities | 2 |
| 180 | 209 | rockets exhausting | 1 |
| 181 | 210 | shallow water | 2 |
| 182 | 211 | gravity location | 3 |
| 183 | 212 | constant temp | 10 |
| 184 | 213 | continuous beams | 1 |
| 185 | 214 | double slotted | 1 |
| 186 | 215 | circular capillary | 1 |
| 187 | 216 | technical note | 4 |
| 188 | 219 | solved numerically | 4 |
| 189 | 220 | correction term | 2 |
| 190 | 221 | km sec | 2 |
| 191 | 222 | reasonable estimates | 2 |
| 192 | 223 | practical purposes | 5 |
| 193 | 224 | purpose analogue | 1 |
| 194 | 225 | represent closely | 2 |
| 195 | 226 | asymmetrical bending | 1 |
| 196 | 227 | planform double | 1 |
| 197 | 228 | nacelle propeller | 1 |
| 198 | 229 | drag programs | 1 |
| 199 | 230 | imperfect gases | 2 |
| 200 | 231 | load capacities | 1 |
| 201 | 232 | circling case | 1 |
| 202 | 233 | air foils | 3 |
| 203 | 235 | considerable interest | 5 |
| 204 | 236 | lower fins | 1 |
| 205 | 237 | magnetic field | 26 |
| 206 | 238 | hole diameter | 2 |
| 207 | 239 | calibration factors | 1 |
| 208 | 240 | radial coordinate | 2 |
| 209 | 241 | torispherical shells | 2 |
| 210 | 242 | kinetic energy | 5 |
| 211 | 243 | static peripheral | 1 |
| 212 | 244 | caret wings | 1 |
| 213 | 245 | fighter type | 1 |
| 214 | 246 | engineering relations | 1 |
| 215 | 247 | liquid nitrogen | 2 |
| 216 | 248 | area surrounding | 1 |
| 217 | 250 | adiabatic recovery | 1 |
| 218 | 251 | mathematical formulation | 2 |
| 219 | 252 | eliminating flutter | 2 |
| 220 | 253 | deformation theories | 4 |
| 221 | 254 | destabilizing influence | 1 |
| 222 | 255 | jet billowing | 1 |
| 223 | 256 | major portion | 4 |
| 224 | 257 | involving initially | 2 |
| 225 | 258 | reference enthalpy | 3 |
| 226 | 259 | substantial reduction | 3 |
| 227 | 261 | spectrum line | 1 |
| 228 | 262 | yawed infinite | 1 |
| 229 | 263 | thermal conductivity | 7 |
| 230 | 264 | downstream movement | 1 |
| 231 | 265 | perpendicularly form | 1 |
| 232 | 266 | core sandwich | 1 |
| 233 | 267 | conductive heat | 2 |
| 234 | 268 | stationary vorticity | 1 |
| 235 | 269 | unstable equilibrium | 1 |
| 236 | 270 | oscillating aerofoil | 1 |
| 237 | 271 | forward fuselage | 1 |
| 238 | 272 | meridional plane | 2 |
| 239 | 273 | velocity squared | 1 |
| 240 | 274 | rear portion | 1 |
| 241 | 275 | thermodynamic transport | 1 |
| 242 | 276 | sonic line | 7 |
| 243 | 277 | inclined bodies | 4 |
| 244 | 278 | axis locations | 1 |
| 245 | 279 | simple quadrature | 2 |
| 246 | 280 | free convection | 13 |
| 247 | 281 | jet issuing | 2 |
| 248 | 283 | compressor operation | 2 |
| 249 | 284 | ft altitude | 1 |
| 250 | 286 | reaction rates | 5 |
| 251 | 287 | forebody length | 2 |
| 252 | 288 | plastic deformation | 2 |
| 253 | 289 | compression corner | 2 |
| 254 | 291 | conical spring | 1 |
| 255 | 293 | theoretical treatments | 3 |
| 256 | 295 | convecting randon | 1 |
| 257 | 296 | cavitating curvilinear | 1 |
| 258 | 298 | computational labor | 1 |
| 259 | 299 | folding wingtip | 1 |
| 260 | 300 | conformal mapping | 4 |
| 261 | 301 | sextic polynomial | 1 |
| 262 | 303 | shroud redesigned | 1 |
| 263 | 304 | chemically reacting | 2 |
| 264 | 305 | overshoot bound | 2 |
| 265 | 306 | orbital period | 5 |
| 266 | 307 | propagating flame | 1 |
| 267 | 308 | multipropeller vtol | 1 |
| 268 | 309 | reentry glider | 2 |
| 269 | 310 | combustion products | 3 |
| 270 | 311 | aerodynamically heated | 4 |
| 271 | 312 | sudden freezing | 1 |
| 272 | 314 | optimum zoom | 1 |
| 273 | 315 | airplane weights | 2 |
| 274 | 316 | varies exponentially | 1 |
| 275 | 317 | hub shroud | 2 |
| 276 | 319 | positive ion | 1 |
| 277 | 320 | axes perpendicular | 1 |
| 278 | 321 | regions terminated | 2 |
| 279 | 322 | strongly dependent | 2 |
| 280 | 323 | naca technical | 2 |
| 281 | 324 | elevated temperatures | 3 |
| 282 | 325 | rheological behaviour | 1 |
| 283 | 326 | miss distance | 2 |
| 284 | 328 | engineering purposes | 3 |
| 285 | 329 | tangency condition | 2 |
| 286 | 331 | arbitrarily prescribed | 2 |
| 287 | 332 | dependent drags | 1 |
| 288 | 333 | specific impulse | 1 |
| 289 | 334 | rectangular ducts | 1 |
| 290 | 335 | essential feature | 2 |
| 291 | 336 | heated driver | 2 |
| 292 | 337 | greatly affected | 4 |
| 293 | 338 | sudden unit | 2 |
| 294 | 339 | fields embedded | 1 |
| 295 | 340 | physical mechanisms | 2 |
| 296 | 341 | considerable simplification | 1 |
| 297 | 342 | fully merged | 2 |
| 298 | 344 | report describes | 10 |
| 299 | 345 | tabular form | 2 |
| 300 | 346 | blunted noses | 1 |
| 301 | 347 | part iv | 2 |
| 302 | 348 | deflected slipstream | 2 |
| 303 | 349 | boundaries characterized | 1 |
| 304 | 350 | spanwise stations | 2 |
| 305 | 351 | existing literature | 2 |
| 306 | 352 | retarding force | 2 |
| 307 | 353 | aft portion | 1 |
| 308 | 354 | significant contribution | 2 |
| 309 | 355 | prescribed loadings | 1 |
| 310 | 357 | untwisted wings | 2 |
| 311 | 358 | closely approaches | 2 |
| 312 | 359 | stratiform bodies | 2 |
| 313 | 361 | perigee altitude | 2 |
| 314 | 363 | practical significance | 3 |
| 315 | 364 | diurnal density | 1 |
| 316 | 365 | sublimation rates | 1 |
| 317 | 366 | integrals involved | 1 |
| 318 | 367 | blast wave | 14 |
| 319 | 368 | relaxation times | 4 |
| 320 | 369 | definite increase | 1 |
| 321 | 370 | solving partial | 1 |
| 322 | 371 | jet plume | 1 |
| 323 | 372 | polar missile | 1 |
| 324 | 373 | acoustic fatigue | 4 |
| 325 | 374 | disturbed region | 1 |
| 326 | 375 | frictional force | 1 |
| 327 | 376 | ballistic missile | 1 |
| 328 | 377 | engineering applications | 2 |
| 329 | 378 | truncated conical | 1 |
| 330 | 379 | room temperature | 4 |
| 331 | 380 | sphere flying | 2 |
| 332 | 382 | modified impellers | 1 |
| 333 | 383 | completely satisfactory | 2 |
| 334 | 384 | external hydrostatic | 2 |
| 335 | 385 | single stage | 4 |
| 336 | 386 | neumann problem | 1 |
| 337 | 387 | light weight | 2 |
| 338 | 388 | dissociation recombination | 2 |
| 339 | 389 | infinite sheet | 2 |
| 340 | 390 | graphical approximation | 1 |
| 341 | 391 | cylindrical shell | 24 |
| 342 | 392 | stiffened cylinders | 4 |
| 343 | 393 | atmospheric entry | 3 |
| 344 | 395 | major source | 1 |
| 345 | 396 | dimensionless parameters | 1 |
| 346 | 397 | side jets | 1 |
| 347 | 398 | compressor stall | 3 |
| 348 | 399 | cruciform column | 1 |
| 349 | 400 | report discusses | 2 |
| 350 | 401 | random processes | 2 |
| 351 | 402 | direct aileron | 1 |
| 352 | 404 | cold solid | 1 |
| 353 | 405 | creep buckling | 25 |
| 354 | 406 | perigee height | 2 |
| 355 | 407 | solid jets | 1 |
| 356 | 408 | blunted cones | 7 |
| 357 | 409 | shock envelopes | 1 |
| 358 | 411 | collapse time | 3 |
| 359 | 412 | obtaining ablation | 1 |
| 360 | 413 | viscous wakes | 3 |
| 361 | 415 | qualitative discussion | 2 |
| 362 | 416 | research program | 3 |
| 363 | 417 | power spectrum | 2 |
| 364 | 418 | lowest reynolds | 5 |
| 365 | 419 | roughly uniform | 1 |
| 366 | 420 | dissociated gases | 1 |
| 367 | 421 | undissociated air | 2 |
| 368 | 422 | air intakes | 1 |
| 369 | 423 | drum camera | 1 |
| 370 | 424 | drawing board | 1 |
| 371 | 425 | boat tailing | 2 |
| 372 | 426 | angularly misaligned | 1 |
| 373 | 427 | cm hg | 1 |
| 374 | 428 | piece wise | 1 |
| 375 | 429 | braking impulse | 1 |
| 376 | 430 | photo thermoelastic | 3 |
| 377 | 431 | kutta joukowski | 2 |
| 378 | 432 | unified viewpoint | 2 |
| 379 | 433 | bomber airplanes | 1 |
| 380 | 434 | solar proton | 1 |
| 381 | 435 | falkner skan | 4 |
| 382 | 436 | skewed parabolic | 1 |
| 383 | 439 | notch depth | 2 |
| 384 | 440 | violet radiation | 1 |
| 385 | 441 | torsional stiffnesses | 1 |
| 386 | 442 | atom recombination | 3 |
| 387 | 443 | thermo aeroelastic | 1 |
| 388 | 444 | stepwise integration | 2 |
| 389 | 446 | partially ionized | 3 |
| 390 | 447 | turbojet powered | 1 |
| 391 | 448 | infinitesimal sides | 2 |
| 392 | 449 | cent probability | 1 |
| 393 | 450 | isentropic exponent | 2 |
| 394 | 452 | strain gage | 2 |
| 395 | 453 | recent advances | 5 |
| 396 | 454 | proof testing | 3 |
| 397 | 455 | simply supported | 29 |
| 398 | 456 | stage stacking | 3 |
| 399 | 457 | hard sphere | 1 |
| 400 | 458 | inlet stages | 2 |
| 401 | 460 | computing machine | 4 |
| 402 | 461 | stepdown height | 1 |
| 403 | 462 | partial conic | 1 |
| 404 | 463 | ft sec | 9 |
| 405 | 464 | tapered holes | 1 |
| 406 | 465 | stage matching | 3 |
| 407 | 467 | column lifetime | 1 |
| 408 | 468 | load meter | 1 |
| 409 | 469 | boat tail | 1 |
| 410 | 470 | positive incremental | 2 |
| 411 | 473 | forced convective | 1 |
| 412 | 474 | successive approximations | 4 |
| 413 | 475 | forced convection | 3 |
| 414 | 477 | local linearisation | 1 |
| 415 | 478 | power output | 3 |
| 416 | 479 | slow oscillations | 2 |
| 417 | 480 | partial differential | 20 |
| 418 | 481 | alternative formulation | 1 |
| 419 | 482 | slot width | 1 |
| 420 | 483 | distinct types | 2 |
| 421 | 484 | single eighth | 2 |
| 422 | 485 | definite set | 2 |
| 423 | 486 | ground proximity | 2 |
| 424 | 487 | paper reviews | 2 |
| 425 | 488 | magneto aerodynamics | 1 |
| 426 | 489 | recent years | 4 |
| 427 | 490 | employing nitrogen | 1 |
| 428 | 491 | thin walled | 19 |
| 429 | 492 | moderate incidences | 2 |
| 430 | 493 | transformed coordinates | 1 |
| 431 | 494 | exit diameters | 4 |
| 432 | 495 | telegraph equation | 2 |
| 433 | 496 | determinantal equation | 1 |
| 434 | 498 | trigonometric series | 2 |
| 435 | 500 | points consisted | 1 |
| 436 | 501 | fourier series | 5 |
| 437 | 502 | analytically expressed | 1 |
| 438 | 504 | mentioned authors | 2 |
| 439 | 505 | noninclined bodies | 1 |
| 440 | 506 | dissociating gas | 3 |
| 441 | 508 | transonic blowdown | 2 |
| 442 | 509 | apparent mass | 4 |
| 443 | 510 | loading margin | 2 |
| 444 | 511 | elastic restraint | 2 |
| 445 | 512 | magnetic fields | 8 |
| 446 | 513 | chemical kinetic | 2 |
| 447 | 514 | interplanetary flight | 2 |
| 448 | 515 | fixing transition | 2 |
| 449 | 516 | pressurized ballistic | 2 |
| 450 | 517 | alloy panels | 1 |
| 451 | 518 | jet plumes | 1 |
| 452 | 519 | important feature | 4 |
| 453 | 520 | annular nozzles | 2 |
| 454 | 521 | loading cycles | 1 |
| 455 | 522 | ablating surfaces | 1 |
| 456 | 523 | blowdown type | 2 |
| 457 | 524 | simpler modes | 1 |
| 458 | 525 | substantially independent | 2 |
| 459 | 526 | eigenvalue problem | 2 |
| 460 | 527 | inch langley | 2 |
| 461 | 528 | laminar bounary | 1 |
| 462 | 529 | energy release | 1 |
| 463 | 530 | vertex angle | 1 |
| 464 | 531 | decreases rapidly | 1 |
| 465 | 532 | stage stall | 2 |
| 466 | 533 | gravitational effects | 2 |
| 467 | 534 | subsonic turbulen | 1 |
| 468 | 535 | mathematical treatment | 2 |
| 469 | 537 | resultant pitching | 2 |
| 470 | 538 | important role | 2 |
| 471 | 539 | tilt wing | 9 |
| 472 | 540 | structure excited | 1 |
| 473 | 541 | extreme cooling | 1 |
| 474 | 542 | physical constants | 1 |
| 475 | 543 | thermal protection | 1 |
| 476 | 544 | positive correlation | 1 |
| 477 | 545 | discontinuity stresses | 2 |
| 478 | 546 | closed end | 1 |
| 479 | 547 | test code | 1 |
| 480 | 548 | gas mixtures | 2 |
| 481 | 549 | double asymptotic | 1 |
| 482 | 551 | geometrically similar | 1 |
| 483 | 552 | buckled rectangular | 2 |
| 484 | 553 | cruciform tail | 2 |
| 485 | 554 | fourth order | 5 |
| 486 | 555 | adjacent surfaces | 2 |
| 487 | 557 | multiweb wing | 2 |
| 488 | 558 | turbulen flows | 1 |
| 489 | 559 | parameter describing | 2 |
| 490 | 560 | intermediate vertical | 1 |
| 491 | 561 | large eddies | 2 |
| 492 | 562 | heat transfer | 174 |
| 493 | 564 | electrically heated | 2 |
| 494 | 565 | piston technique | 1 |
| 495 | 566 | formulas relating | 1 |
| 496 | 567 | analytical formulation | 2 |
| 497 | 568 | logarithmic decrement | 1 |
| 498 | 569 | turbo machines | 1 |
| 499 | 570 | vertex centered | 1 |
| 500 | 571 | tollmien schlichting | 3 |
| 501 | 572 | descent phases | 1 |
| 502 | 573 | deepest corridor | 1 |
| 503 | 574 | shuffle reactions | 1 |
| 504 | 575 | taylor maccoll | 3 |
| 505 | 577 | agrees perfectly | 2 |
| 506 | 579 | navier stokes | 19 |
| 507 | 580 | schlieren pictures | 3 |
| 508 | 581 | variational theorems | 1 |
| 509 | 582 | slotted flaps | 1 |
| 510 | 583 | pump impellers | 1 |
| 511 | 584 | finding eigenvalues | 1 |
| 512 | 585 | conpressibility transformation | 1 |
| 513 | 586 | fundamental shortcomings | 1 |
| 514 | 587 | varies inversely | 3 |
| 515 | 588 | sinusoidal sinking | 1 |
| 516 | 589 | structural joints | 2 |
| 517 | 590 | essential difficulty | 2 |
| 518 | 591 | discontinuous middle | 1 |
| 519 | 592 | sting mounted | 2 |
| 520 | 593 | spherical cap | 3 |
| 521 | 594 | ethylene heated | 2 |
| 522 | 595 | engined vertical | 1 |
| 523 | 596 | arrhenius law | 2 |
| 524 | 597 | stiffened longitudinally | 1 |
| 525 | 598 | wedge shaped | 3 |
| 526 | 599 | infinitely long | 9 |
| 527 | 600 | entry mission | 1 |
| 528 | 601 | rotor blades | 1 |
| 529 | 602 | transonic bump | 1 |
| 530 | 603 | surge phenomena | 1 |
| 531 | 604 | approaches infinity | 2 |
| 532 | 605 | creeping motion | 1 |
| 533 | 606 | bell type | 1 |
| 534 | 607 | nickel base | 1 |
| 535 | 608 | tailplane combination | 1 |
| 536 | 609 | alternative forms | 1 |
| 537 | 610 | double wedge | 3 |
| 538 | 612 | random excitation | 1 |
| 539 | 613 | part iii | 3 |
| 540 | 614 | roughness capable | 1 |
| 541 | 615 | obvious practical | 2 |
| 542 | 617 | conducting fluids | 3 |
| 543 | 618 | iteration processes | 1 |
| 544 | 619 | landing airplane | 1 |
| 545 | 620 | axially symmetrical | 5 |
| 546 | 621 | atmosphere entries | 2 |
| 547 | 622 | preston tube | 2 |
| 548 | 623 | quantitative estimates | 1 |
| 549 | 624 | strictly inviscid | 1 |
| 550 | 625 | sectorial plates | 2 |
| 551 | 626 | slowly varying | 2 |
| 552 | 627 | vtol aircraft | 5 |
| 553 | 628 | generalized coordinates | 3 |
| 554 | 629 | rolling missile | 2 |
| 555 | 630 | plastic deformations | 3 |
| 556 | 631 | upper atmosphere | 7 |
| 557 | 632 | finite slabs | 2 |
| 558 | 633 | progress report | 1 |
| 559 | 634 | initial imperfection | 1 |
| 560 | 635 | rocket exhaust | 4 |
| 561 | 636 | front stages | 2 |
| 562 | 637 | transport properties | 9 |
| 563 | 638 | reflection process | 2 |
| 564 | 640 | yield substantially | 2 |
| 565 | 641 | maximum deceleration | 4 |
| 566 | 642 | semivertex angle | 6 |
| 567 | 643 | vary linearly | 2 |
| 568 | 644 | exploratory studies | 2 |
| 569 | 645 | jet inoperative | 1 |
| 570 | 646 | schlichting waves | 1 |
| 571 | 647 | propulsion system | 3 |
| 572 | 648 | glide configurations | 1 |
| 573 | 649 | square lattices | 1 |
| 574 | 650 | aerothermoelastic similarity | 1 |
| 575 | 651 | transverse magnetic | 11 |
| 576 | 652 | panels exposed | 2 |
| 577 | 653 | edge tractions | 1 |
| 578 | 655 | real gas | 16 |
| 579 | 656 | molecular vibration | 3 |
| 580 | 658 | similarity law | 5 |
| 581 | 660 | varying linearly | 2 |
| 582 | 661 | column matrix | 1 |
| 583 | 662 | relaxation oscillations | 1 |
| 584 | 663 | fineness ratio | 16 |
| 585 | 665 | successful application | 2 |
| 586 | 666 | paper deals | 8 |
| 587 | 667 | imposed magnetic | 2 |
| 588 | 668 | supersonic diffusers | 1 |
| 589 | 669 | vertical acceleration | 3 |
| 590 | 670 | materials tested | 1 |
| 591 | 671 | author considers | 2 |
| 592 | 672 | control hinge | 2 |
| 593 | 673 | tumbling motion | 2 |
| 594 | 674 | square inch | 1 |
| 595 | 675 | considerably greater | 4 |
| 596 | 676 | elastic constants | 4 |
| 597 | 677 | tail surfaces | 4 |
| 598 | 678 | variable geometry | 3 |
| 599 | 679 | highly loaded | 1 |
| 600 | 681 | slender cruciform | 3 |
| 601 | 682 | landing aircraft | 1 |
| 602 | 683 | ultra high | 1 |
| 603 | 684 | tip radius | 2 |
| 604 | 685 | fineness ratios | 4 |
| 605 | 686 | leads directly | 2 |
| 606 | 687 | cylindrical sting | 2 |
| 607 | 688 | core positions | 1 |
| 608 | 689 | obtaining asymptotic | 1 |
| 609 | 690 | bring transition | 1 |
| 610 | 691 | causing separation | 2 |
| 611 | 692 | compressive stress | 7 |
| 612 | 693 | good qualitative | 4 |
| 613 | 694 | injected gas | 4 |
| 614 | 695 | normal force | 21 |
| 615 | 696 | aec univac | 2 |
| 616 | 699 | multiply connected | 2 |
| 617 | 700 | elastically restrained | 1 |
| 618 | 701 | national advisory | 2 |
| 619 | 703 | btu lb | 3 |
| 620 | 706 | sinusoidal gusts | 1 |
| 621 | 707 | geometrical acoustics | 1 |
| 622 | 708 | terminal guidance | 1 |
| 623 | 709 | automatic recording | 1 |
| 624 | 710 | electrical analogies | 1 |
| 625 | 711 | unsteadily rotating | 1 |
| 626 | 713 | ascending powers | 2 |
| 627 | 714 | von mises | 5 |
| 628 | 715 | sheltered side | 1 |
| 629 | 716 | economical missile | 1 |
| 630 | 718 | rapidly freeze | 1 |
| 631 | 719 | caloric imperfections | 1 |
| 632 | 720 | controlled trail | 1 |
| 633 | 722 | electronic apparatus | 1 |
| 634 | 723 | systematic group | 1 |
| 635 | 724 | simply supplorted | 1 |
| 636 | 725 | freely supported | 2 |
| 637 | 729 | centrally loaded | 1 |
| 638 | 731 | straight edged | 1 |
| 639 | 732 | blade rows | 4 |
| 640 | 733 | compressor surge | 2 |
| 641 | 734 | semicircular cross | 1 |
| 642 | 735 | moderately thick | 1 |
| 643 | 737 | author obtains | 2 |
| 644 | 739 | stressing heated | 1 |
| 645 | 740 | mangler transformation | 2 |
| 646 | 741 | horseshoe vortex | 2 |
| 647 | 742 | thrust vector | 4 |
| 648 | 743 | hinge locations | 1 |
| 649 | 744 | automatic computers | 1 |
| 650 | 746 | vortex cancellation | 1 |
| 651 | 747 | creep rupture | 2 |
| 652 | 748 | redundant structures | 1 |
| 653 | 749 | semiapex angles | 3 |
| 654 | 751 | improved smoke | 1 |
| 655 | 752 | difficulties arising | 2 |
| 656 | 753 | gross radial | 1 |
| 657 | 754 | axi symmetric | 1 |
| 658 | 755 | generalised porous | 2 |
| 659 | 756 | rheological approach | 1 |
| 660 | 757 | considerable fraction | 2 |
| 661 | 758 | control devices | 1 |
| 662 | 759 | turbine lattices | 1 |
| 663 | 760 | nonequilibrium dissociating | 1 |
| 664 | 761 | reentry ballistic | 1 |
| 665 | 762 | planetary atmosphere | 3 |
| 666 | 764 | data processing | 2 |
| 667 | 765 | glide vehicles | 2 |
| 668 | 767 | supply system | 1 |
| 669 | 768 | corridor width | 1 |
| 670 | 770 | discharge coefficient | 2 |
| 671 | 771 | solid construction | 2 |
| 672 | 772 | thermal cycling | 1 |
| 673 | 773 | conduction controlled | 1 |
| 674 | 774 | methods fore | 1 |
| 675 | 775 | post buckling | 4 |
| 676 | 776 | square planform | 2 |
| 677 | 777 | base bleed | 2 |
| 678 | 778 | section stringers | 1 |
| 679 | 780 | plan form | 12 |
| 680 | 781 | inelastic systems | 1 |
| 681 | 782 | attachment line | 2 |
| 682 | 783 | entry trajectories | 2 |
| 683 | 784 | mathieu function | 1 |
| 684 | 785 | helium simulation | 1 |
| 685 | 786 | ellipse cylinder | 1 |
| 686 | 787 | curves showing | 3 |
| 687 | 788 | roughness particles | 2 |
| 688 | 789 | buckled panel | 5 |
| 689 | 790 | author discusses | 1 |
| 690 | 791 | linearly varying | 2 |
| 691 | 792 | coordinate system | 3 |
| 692 | 793 | future research | 2 |
| 693 | 795 | perforated tunnel | 1 |
| 694 | 796 | wide ranges | 2 |
| 695 | 797 | overexpanded nozzle | 1 |
| 696 | 798 | natural frequency | 3 |
| 697 | 800 | longitudinal stiffeners | 1 |
| 698 | 801 | block ratio | 1 |
| 699 | 802 | sample calculation | 4 |
| 700 | 803 | gas dynamics | 4 |
| 701 | 804 | tilting wing | 3 |
| 702 | 805 | inelastic structures | 1 |
| 703 | 806 | thermal stresses | 15 |
| 704 | 807 | powered aircraft | 1 |
| 705 | 808 | cylinder juncture | 1 |
| 706 | 810 | paper concludes | 2 |
| 707 | 811 | significantly lower | 2 |
| 708 | 812 | swept wings | 10 |
| 709 | 813 | rectangular plan | 1 |
| 710 | 815 | mode shapes | 6 |
| 711 | 816 | conical afterbodies | 1 |
| 712 | 818 | large proportion | 2 |
| 713 | 819 | stress strain | 9 |
| 714 | 820 | rotor incidence | 1 |
| 715 | 821 | previous investigations | 2 |
| 716 | 822 | stresses arising | 1 |
| 717 | 823 | symmetric deformations | 1 |
| 718 | 824 | destabilizing effect | 4 |
| 719 | 825 | ethylene air | 1 |
| 720 | 826 | chapman jouguet | 1 |
| 721 | 827 | van gorcum | 1 |
| 722 | 829 | refractory shield | 1 |
| 723 | 830 | chemically active | 3 |
| 724 | 831 | permanent perturbation | 1 |
| 725 | 832 | statically stable | 4 |
| 726 | 833 | depend critically | 3 |
| 727 | 834 | corridor widths | 1 |
| 728 | 835 | remains invariant | 2 |
| 729 | 837 | naca rm | 3 |
| 730 | 838 | solar ultra | 1 |
| 731 | 839 | electric analog | 2 |
| 732 | 840 | nasa technical | 2 |
| 733 | 841 | moving parallell | 1 |
| 734 | 842 | physical interpretations | 1 |
| 735 | 843 | analytic continuation | 2 |
| 736 | 844 | corridor depth | 2 |
| 737 | 845 | finding roots | 1 |
| 738 | 846 | diving moments | 2 |
| 739 | 847 | pressurised ring | 1 |
| 740 | 849 | crocco lees | 2 |
| 741 | 850 | digital computer | 7 |
| 742 | 852 | uniquely dependent | 1 |
| 743 | 853 | infinite expanse | 1 |
| 744 | 854 | anti symmetric | 1 |
| 745 | 855 | full skirted | 1 |
| 746 | 856 | parabolic blading | 1 |
| 747 | 857 | satellite orbits | 6 |
| 748 | 858 | sudden contact | 1 |
| 749 | 859 | wider applicability | 1 |
| 750 | 861 | poor intermediate | 2 |
| 751 | 863 | vertical stabilizer | 1 |
| 752 | 864 | airfoil crest | 1 |
| 753 | 865 | satellite traversing | 1 |
| 754 | 866 | noise signals | 1 |
| 755 | 868 | airplane attitude | 1 |
| 756 | 869 | continuous ignition | 1 |
| 757 | 870 | lateral directions | 1 |
| 758 | 871 | nonconducting walls | 2 |
| 759 | 872 | single bay | 1 |
| 760 | 873 | split flaps | 2 |
| 761 | 874 | flaps deflected | 2 |
| 762 | 875 | uncoupled mode | 1 |
| 763 | 876 | sphere inside | 1 |
| 764 | 877 | isotropic turbulence | 2 |
| 765 | 879 | sharp edged | 3 |
| 766 | 880 | tangent wedge | 7 |
| 767 | 881 | minor axis | 2 |
| 768 | 882 | semi empirical | 6 |
| 769 | 883 | rotation term | 1 |
| 770 | 884 | controlled laboratory | 2 |
| 771 | 885 | short oval | 1 |
| 772 | 886 | fourth root | 2 |
| 773 | 887 | peak stiffener | 1 |
| 774 | 888 | paper summarizes | 2 |
| 775 | 889 | redundant structure | 1 |
| 776 | 890 | stress resultants | 1 |
| 777 | 891 | limited amount | 5 |
| 778 | 892 | mathematical difficulties | 2 |
| 779 | 893 | close proximity | 3 |
| 780 | 894 | local dynamical | 1 |
| 781 | 895 | tip fins | 1 |
| 782 | 896 | compressor routine | 1 |
| 783 | 897 | favor part | 2 |
| 784 | 898 | solved explicitly | 2 |
| 785 | 899 | solid fuel | 1 |
| 786 | 900 | sobsonic speeds | 1 |
| 787 | 901 | configuration consisting | 1 |
| 788 | 902 | recent contribution | 2 |
| 789 | 903 | failing stress | 2 |
| 790 | 904 | air scooping | 1 |
| 791 | 905 | cruise performance | 1 |
| 792 | 906 | parallel streams | 4 |
| 793 | 907 | ordinary differential | 13 |
| 794 | 908 | iterative process | 4 |
| 795 | 909 | stiffness matrix | 1 |
| 796 | 910 | pertinent expressions | 1 |
| 797 | 911 | working fluids | 1 |
| 798 | 912 | reacting gas | 2 |
| 799 | 913 | discrete frequency | 2 |
| 800 | 914 | jet pluming | 1 |
| 801 | 915 | empirical information | 2 |
| 802 | 916 | negative damping | 2 |
| 803 | 917 | knuckle region | 1 |
| 804 | 918 | plastic torsional | 1 |
| 805 | 920 | entry trajectory | 2 |
| 806 | 921 | modulated entry | 1 |
| 807 | 922 | powered flight | 1 |
| 808 | 923 | electron density | 3 |
| 809 | 924 | classical criterion | 1 |
| 810 | 925 | thick walls | 1 |
| 811 | 926 | downwash surveys | 1 |
| 812 | 927 | major components | 2 |
| 813 | 928 | median section | 1 |
| 814 | 929 | camber deflections | 1 |
| 815 | 931 | variational formulation | 1 |
| 816 | 932 | toroidal shell | 1 |
| 817 | 933 | adiabatic wall | 9 |
| 818 | 934 | rectangular cantilever | 2 |
| 819 | 935 | versus time | 2 |
| 820 | 936 | extensive series | 3 |
| 821 | 937 | helium injection | 8 |
| 822 | 938 | tip bluntness | 2 |
| 823 | 939 | length width | 3 |
| 824 | 940 | transtability flutter | 1 |
| 825 | 941 | allowable axial | 1 |
| 826 | 942 | wave advancing | 2 |
| 827 | 943 | taper ratio | 8 |
| 828 | 944 | techniques applying | 1 |
| 829 | 945 | great practical | 2 |
| 830 | 946 | aircraft structures | 9 |
| 831 | 947 | shock standoff | 2 |
| 832 | 948 | incremental normal | 2 |
| 833 | 949 | stationary convection | 1 |
| 834 | 950 | nose radii | 2 |
| 835 | 951 | pivotal point | 2 |
| 836 | 952 | reasonable accuracy | 3 |
| 837 | 953 | transonic dynamics | 1 |
| 838 | 954 | prevent flutter | 2 |
| 839 | 955 | conical afterbody | 6 |
| 840 | 956 | saunders roe | 1 |
| 841 | 958 | jmin erfc | 1 |
| 842 | 959 | slider bearing | 1 |
| 843 | 960 | reviewer feels | 2 |
| 844 | 961 | photo thermoelasticity | 1 |
| 845 | 962 | specialized situations | 1 |
| 846 | 963 | stainless steel | 3 |
| 847 | 964 | splitter vane | 1 |
| 848 | 965 | lb sq | 2 |
| 849 | 966 | discoverer satellites | 1 |
| 850 | 967 | glass shields | 1 |
| 851 | 968 | gaseous detonation | 1 |
| 852 | 970 | proved inadequate | 2 |
| 853 | 971 | naca rep | 4 |
| 854 | 972 | planetary atmospheres | 3 |
| 855 | 974 | plastics teflon | 1 |
| 856 | 976 | inversely proportional | 2 |
| 857 | 977 | aerelastic considerations | 1 |
| 858 | 978 | naca tn | 6 |
| 859 | 979 | windward generator | 1 |
| 860 | 980 | nodal pattern | 3 |
| 861 | 981 | guidance requirements | 2 |
| 862 | 982 | magneto hydrodynamic | 2 |
| 863 | 983 | downwash impingement | 1 |
| 864 | 986 | artificial satellites | 2 |
| 865 | 987 | identical equally | 1 |
| 866 | 988 | hot wires | 3 |
| 867 | 989 | ring stiffened | 9 |
| 868 | 990 | strain gages | 2 |
| 869 | 991 | exit staticpressure | 1 |
| 870 | 992 | analog computer | 1 |
| 871 | 994 | wetted area | 1 |
| 872 | 995 | wingtip panels | 2 |
| 873 | 996 | oblate atmosphere | 2 |
| 874 | 997 | tumbling motions | 1 |
| 875 | 998 | edges elastically | 3 |
| 876 | 999 | semi ellipsoidal | 1 |
| 877 | 1000 | gaussian curvature | 2 |
| 878 | 1001 | round entrance | 1 |
| 879 | 1003 | prior knowledge | 2 |
| 880 | 1004 | main text | 2 |
| 881 | 1006 | sodium line | 2 |
| 882 | 1007 | windward side | 3 |
| 883 | 1008 | automatic computer | 1 |
| 884 | 1009 | authors discuss | 2 |
| 885 | 1010 | span wise | 2 |
| 886 | 1011 | vibrations excited | 3 |
| 887 | 1014 | running times | 2 |
| 888 | 1015 | atmospheric entries | 1 |
| 889 | 1016 | oseen linearization | 1 |
| 890 | 1018 | single pass | 2 |
| 891 | 1019 | semi infinite | 16 |
| 892 | 1020 | analogue computer | 2 |
| 893 | 1021 | circumferential band | 2 |
| 894 | 1022 | flexural vibrations | 2 |
| 895 | 1023 | time histories | 7 |
| 896 | 1024 | rendering approximate | 1 |
| 897 | 1025 | increasingly important | 1 |
| 898 | 1026 | infinitesimally thin | 2 |
| 899 | 1027 | entering planetary | 1 |
| 900 | 1028 | increases linearly | 5 |
| 901 | 1029 | reentry configuration | 2 |
| 902 | 1030 | pitot tubes | 4 |
| 903 | 1031 | blunt nosed | 22 |
| 904 | 1032 | proceeds downstream | 2 |
| 905 | 1033 | fourth power | 6 |
| 906 | 1034 | effective heats | 3 |
| 907 | 1035 | transverse vibrations | 7 |
| 908 | 1036 | elongated bodies | 1 |
| 909 | 1037 | uniformly valid | 3 |
| 910 | 1038 | double beam | 1 |
| 911 | 1040 | complementary function | 1 |
| 912 | 1041 | fundamental concepts | 2 |
| 913 | 1042 | supporting structure | 3 |
| 914 | 1043 | hemispherical nose | 4 |
| 915 | 1044 | unstiffened circular | 1 |
| 916 | 1045 | pressurized cylinders | 6 |
| 917 | 1046 | leading edge | 89 |
| 918 | 1047 | diatomic gas | 4 |
| 919 | 1048 | desired degree | 2 |
| 920 | 1049 | spin rate | 1 |
| 921 | 1050 | multistage axial | 2 |
| 922 | 1051 | partially porous | 1 |
| 923 | 1052 | forebody vortices | 1 |
| 924 | 1053 | discontinuous profile | 1 |
| 925 | 1054 | noncatalytic wall | 2 |
| 926 | 1055 | overexpanded conical | 1 |
| 927 | 1056 | real fluids | 2 |
| 928 | 1057 | reflected head | 1 |
| 929 | 1058 | sideslip derivatives | 2 |
| 930 | 1059 | variables covered | 2 |
| 931 | 1060 | circular sector | 1 |
| 932 | 1061 | thermodynamic equilibrium | 8 |
| 933 | 1062 | side force | 5 |
| 934 | 1063 | reattaching flows | 1 |
| 935 | 1064 | flared cylinder | 1 |
| 936 | 1065 | shearing forces | 2 |
| 937 | 1066 | fully developed | 10 |
| 938 | 1067 | buckled panels | 3 |
| 939 | 1068 | incremental theories | 3 |
| 940 | 1069 | resultant force | 4 |
| 941 | 1070 | simulated rocket | 1 |
| 942 | 1071 | sudden change | 2 |
| 943 | 1072 | midplane stress | 2 |
| 944 | 1073 | radial displacements | 2 |
| 945 | 1074 | escape speed | 2 |
| 946 | 1075 | supersonic turbo | 1 |
| 947 | 1076 | compressor blades | 2 |
| 948 | 1077 | studied analytically | 1 |
| 949 | 1078 | stiffened curved | 1 |
| 950 | 1079 | flat plate | 130 |
| 951 | 1081 | trim angles | 2 |
| 952 | 1082 | yawing moment | 1 |
| 953 | 1083 | directional stability | 1 |
| 954 | 1084 | approximate indical | 1 |
| 955 | 1085 | loads program | 1 |
| 956 | 1087 | shock intensities | 1 |
| 957 | 1088 | flexible modes | 2 |
| 958 | 1089 | perturbations due | 1 |
| 959 | 1090 | exponential external | 1 |
| 960 | 1091 | successfully applied | 2 |
| 961 | 1092 | performance estimates | 2 |
| 962 | 1093 | sandwich structures | 1 |
| 963 | 1094 | airfoil sections | 5 |
| 964 | 1095 | observed experimentally | 4 |
| 965 | 1096 | predicting column | 1 |
| 966 | 1097 | chemical equilibrium | 4 |
| 967 | 1099 | hangling qualities | 1 |
| 968 | 1100 | turbulen coundary | 1 |
| 969 | 1101 | circumscribing polygon | 2 |
| 970 | 1103 | bay aluminium | 1 |
| 971 | 1104 | charged conductor | 1 |
| 972 | 1105 | tapered discs | 1 |
| 973 | 1106 | bodt freedom | 1 |
| 974 | 1107 | compare favorably | 2 |
| 975 | 1108 | quick acting | 1 |
| 976 | 1109 | particle entrainment | 1 |
| 977 | 1110 | maritime transport | 1 |
| 978 | 1111 | mechanical stressing | 1 |
| 979 | 1112 | intense explosion | 1 |
| 980 | 1113 | circulation lag | 1 |
| 981 | 1115 | classical identity | 1 |
| 982 | 1116 | ideal dissociating | 7 |
| 983 | 1117 | geometrically orthotropic | 1 |
| 984 | 1118 | tangent modulus | 4 |
| 985 | 1119 | circumferential nodes | 1 |
| 986 | 1120 | prandtl meyer | 6 |
| 987 | 1121 | profiles inafinite | 1 |
| 988 | 1122 | complementary error | 1 |
| 989 | 1123 | retrorocket thrust | 1 |
| 990 | 1124 | kinematic viscosity | 5 |
| 991 | 1125 | corrugated core | 3 |
| 992 | 1126 | factors affecting | 5 |
| 993 | 1127 | driver gases | 2 |
| 994 | 1128 | hugoniot relations | 1 |
| 995 | 1129 | electronic computer | 1 |
| 996 | 1130 | missile descending | 1 |
| 997 | 1131 | points lying | 1 |
| 998 | 1132 | classical hydrodynamics | 2 |
| 999 | 1133 | digital computing | 1 |
| 1000 | 1134 | slipstream downward | 1 |
| 1001 | 1136 | porous plug | 2 |
| 1002 | 1137 | joule heating | 1 |
| 1003 | 1138 | aerothermoelastic testing | 1 |
| 1004 | 1139 | ogive forebody | 1 |
| 1005 | 1141 | blade row | 2 |
| 1006 | 1142 | parabolic arc | 4 |
| 1007 | 1143 | sine curves | 1 |
| 1008 | 1144 | severe acoustic | 1 |
| 1009 | 1145 | author proceeds | 1 |
| 1010 | 1146 | power expenditure | 1 |
| 1011 | 1147 | deflecting propeller | 1 |
| 1012 | 1148 | turbine blades | 3 |
| 1013 | 1149 | hammerhead nose | 1 |
| 1014 | 1150 | debye length | 1 |
| 1015 | 1152 | radially symmetric | 1 |
| 1016 | 1153 | comparable ballistic | 1 |
| 1017 | 1154 | frictional resistance | 1 |
| 1018 | 1155 | transverse stiffeners | 5 |
| 1019 | 1156 | jets exhausting | 2 |
| 1020 | 1157 | engineering materials | 1 |
| 1021 | 1158 | previously published | 3 |
| 1022 | 1159 | attached oblique | 1 |
| 1023 | 1160 | atmospheric reentry | 2 |
| 1024 | 1161 | isentropic streams | 1 |
| 1025 | 1163 | structural matrices | 1 |
| 1026 | 1165 | wave refracts | 1 |
| 1027 | 1166 | round pitot | 1 |
| 1028 | 1167 | elliptic orbit | 3 |
| 1029 | 1168 | engine exhaust | 1 |
| 1030 | 1169 | closed form | 18 |
| 1031 | 1170 | cross plots | 2 |
| 1032 | 1171 | part ii | 4 |
| 1033 | 1172 | compressibility transformation | 3 |
| 1034 | 1173 | good agreement | 66 |
| 1035 | 1174 | plane poiseuille | 1 |
| 1036 | 1175 | hodograph plane | 1 |
| 1037 | 1176 | rocket jets | 2 |
| 1038 | 1177 | thrust production | 1 |
| 1039 | 1178 | methane air | 2 |
| 1040 | 1179 | metals creep | 1 |
| 1041 | 1180 | rotor blade | 1 |
| 1042 | 1181 | rocket propulsion | 1 |
| 1043 | 1182 | middle surfaces | 1 |
| 1044 | 1183 | fatigue failure | 4 |
| 1045 | 1184 | testing machine | 1 |
| 1046 | 1185 | degree sweptback | 3 |
| 1047 | 1186 | factor affecting | 1 |
| 1048 | 1187 | modified strip | 1 |
| 1049 | 1188 | give rise | 7 |
| 1050 | 1189 | random vibration | 2 |
| 1051 | 1190 | degree sweepback | 2 |
| 1052 | 1191 | preliminary estimates | 2 |
| 1053 | 1192 | stagnation enthalpies | 2 |
| 1054 | 1193 | tail locations | 1 |
| 1055 | 1194 | vortex paths | 2 |
| 1056 | 1195 | generally resulted | 2 |
| 1057 | 1196 | cyclic thermal | 1 |
| 1058 | 1197 | local inclination | 1 |
| 1059 | 1198 | biharmonic equation | 1 |
| 1060 | 1199 | discharge coefficients | 2 |
| 1061 | 1200 | nonsimilar solutions | 1 |
| 1062 | 1201 | practical interest | 4 |
| 1063 | 1203 | qualitative information | 1 |
| 1064 | 1204 | generalised newtonian | 1 |
| 1065 | 1205 | turning angle | 4 |
| 1066 | 1206 | gust pattern | 1 |
| 1067 | 1208 | toroidal shells | 1 |
| 1068 | 1209 | outer expansions | 1 |
| 1069 | 1210 | rapid convergence | 2 |
| 1070 | 1211 | adjacent edges | 2 |
| 1071 | 1212 | alfven velocity | 1 |
| 1072 | 1213 | maintaining laminar | 1 |
| 1073 | 1214 | concentration profiles | 1 |
| 1074 | 1215 | cylinder frustum | 1 |
| 1075 | 1216 | matrix force | 2 |
| 1076 | 1217 | initial deviation | 2 |
| 1077 | 1219 | nose blunting | 3 |
| 1078 | 1220 | circular arc | 4 |
| 1079 | 1221 | throat diameter | 2 |
| 1080 | 1222 | report deals | 2 |
| 1081 | 1223 | trailing edges | 9 |
| 1082 | 1224 | closing reply | 1 |
| 1083 | 1226 | confluent hypergeometric | 1 |
| 1084 | 1227 | gauss seidel | 1 |
| 1085 | 1230 | inequality constraints | 1 |
| 1086 | 1231 | rankine hugoniot | 2 |
| 1087 | 1232 | york university | 2 |
| 1088 | 1233 | van driest | 1 |
| 1089 | 1234 | impeller wheel | 1 |
| 1090 | 1235 | wood smoke | 1 |
| 1091 | 1236 | fiber glass | 2 |
| 1092 | 1237 | aluminum alloy | 12 |
| 1093 | 1238 | undershoot bound | 1 |
| 1094 | 1239 | floating element | 4 |
| 1095 | 1240 | engine mounting | 1 |
| 1096 | 1241 | binary scaling | 1 |
| 1097 | 1242 | guide vanes | 2 |
| 1098 | 1243 | question arises | 1 |
| 1099 | 1244 | atomic oxygen | 2 |
| 1100 | 1245 | von karman | 23 |
| 1101 | 1246 | farther back | 2 |
| 1102 | 1247 | flexural rigidity | 3 |
| 1103 | 1248 | isobar pattern | 1 |
| 1104 | 1249 | relating flexure | 1 |
| 1105 | 1250 | breathing vibrations | 2 |
| 1106 | 1252 | axi symmetrical | 1 |
| 1107 | 1253 | highly polished | 1 |
| 1108 | 1254 | shroud contours | 2 |
| 1109 | 1255 | forward facing | 6 |
| 1110 | 1256 | launched rocket | 1 |
| 1111 | 1257 | enclosed area | 1 |
| 1112 | 1258 | short skirted | 1 |
| 1113 | 1260 | oscillating harmonically | 2 |
| 1114 | 1261 | sixth degree | 2 |
| 1115 | 1262 | magnetic inductance | 1 |
| 1116 | 1263 | closely spaced | 1 |
| 1117 | 1264 | projectile related | 1 |
| 1118 | 1265 | moving steadily | 2 |
| 1119 | 1266 | manned vehicles | 4 |
| 1120 | 1268 | periodically oscillating | 1 |
| 1121 | 1269 | controlling stiffness | 1 |
| 1122 | 1270 | integrated numerically | 7 |
| 1123 | 1271 | smallest height | 1 |
| 1124 | 1272 | intrinsic system | 1 |
| 1125 | 1273 | dead weight | 3 |
| 1126 | 1274 | special care | 1 |
| 1127 | 1275 | inert internal | 1 |
| 1128 | 1277 | generally accepted | 2 |
| 1129 | 1278 | charts adapted | 1 |
| 1130 | 1279 | systematic kernel | 1 |
| 1131 | 1280 | prandtl glauert | 4 |
| 1132 | 1281 | forces exerted | 1 |
| 1133 | 1282 | inert mode | 1 |
| 1134 | 1283 | laval nozzle | 1 |
| 1135 | 1284 | varies linearly | 3 |
| 1136 | 1286 | wich cylinders | 1 |
| 1137 | 1287 | lower bound | 2 |
| 1138 | 1288 | mixing zone | 5 |
| 1139 | 1289 | short period | 4 |
| 1140 | 1290 | nonparallel plane | 1 |
| 1141 | 1291 | appreciably affected | 1 |
| 1142 | 1292 | insulating properties | 1 |
| 1143 | 1293 | plates reinforced | 3 |
| 1144 | 1294 | aeronautical research | 2 |
| 1145 | 1295 | thermochemical equilibrium | 2 |
| 1146 | 1296 | unpowered flight | 1 |
| 1147 | 1297 | dissociated hypervelocity | 1 |
| 1148 | 1298 | thermal diffusivity | 1 |
| 1149 | 1299 | bulk viscosity | 1 |
| 1150 | 1301 | major minor | 2 |
| 1151 | 1303 | finite difference | 17 |
| 1152 | 1304 | uniaxial stress | 4 |
| 1153 | 1305 | lowest frequency | 1 |
| 1154 | 1306 | hollow cylinder | 2 |
| 1155 | 1307 | cylindrical membranes | 2 |
| 1156 | 1308 | rotating stall | 2 |
| 1157 | 1309 | dynamic rotary | 1 |
| 1158 | 1311 | criterion applies | 2 |
| 1159 | 1312 | streamline pattern | 3 |
| 1160 | 1313 | excellent agreement | 7 |
| 1161 | 1315 | elliptic integrals | 1 |
| 1162 | 1316 | foreign gas | 8 |
| 1163 | 1318 | meridian section | 1 |
| 1164 | 1319 | satellite orbit | 3 |
| 1165 | 1320 | propeller slipstream | 5 |
| 1166 | 1321 | hinge moment | 3 |
| 1167 | 1322 | strong blast | 1 |
| 1168 | 1324 | delta planform | 2 |
| 1169 | 1325 | negligibly small | 3 |
| 1170 | 1327 | hoop stresses | 2 |
| 1171 | 1328 | galerkin process | 1 |
| 1172 | 1329 | flight path | 10 |
| 1173 | 1330 | pure bending | 5 |
| 1174 | 1331 | open area | 2 |
| 1175 | 1332 | continuous sinusoidal | 1 |
| 1176 | 1333 | theoretically perfect | 1 |
| 1177 | 1334 | volume term | 1 |
| 1178 | 1335 | slender ogee | 1 |
| 1179 | 1336 | roughness sizes | 1 |
| 1180 | 1337 | head forms | 1 |
| 1181 | 1338 | motion pictures | 2 |
| 1182 | 1339 | generalised conical | 2 |
| 1183 | 1340 | nonstationary compressible | 1 |
| 1184 | 1341 | elastic toroidal | 1 |
| 1185 | 1342 | hyperbolic approach | 1 |
| 1186 | 1343 | cylindrical afterbodies | 3 |
| 1187 | 1345 | taking account | 2 |
| 1188 | 1346 | rarefied gas | 4 |
| 1189 | 1347 | tangential loading | 1 |
| 1190 | 1348 | explicit relation | 1 |
| 1191 | 1350 | conical camber | 1 |
| 1192 | 1351 | independent variable | 6 |
| 1193 | 1353 | vibrational equilibrium | 1 |
| 1194 | 1355 | paper concerns | 2 |
| 1195 | 1356 | maxwellian distribution | 2 |
| 1196 | 1357 | briefly discussed | 10 |
| 1197 | 1358 | large negatively | 1 |
| 1198 | 1360 | shroud technique | 2 |
| 1199 | 1361 | provide information | 2 |
| 1200 | 1362 | cantilever square | 1 |
| 1201 | 1363 | modulus material | 1 |
| 1202 | 1365 | lagrange equation | 2 |
| 1203 | 1367 | return lunar | 1 |
| 1204 | 1368 | usaf sponsored | 2 |
| 1205 | 1369 | negatively sloped | 1 |
| 1206 | 1370 | sodium carbonate | 2 |
| 1207 | 1372 | california institute | 3 |
| 1208 | 1373 | crossed flexure | 1 |
| 1209 | 1374 | loose dirt | 1 |
| 1210 | 1375 | transversely impinging | 1 |
| 1211 | 1376 | buried fan | 1 |
| 1212 | 1377 | newton busemann | 2 |
| 1213 | 1378 | rae bedford | 2 |
| 1214 | 1379 | apparent contradictions | 1 |
| 1215 | 1380 | nasa lewis | 2 |
| 1216 | 1381 | aileron buzz | 1 |
| 1217 | 1382 | face wrinkling | 1 |
| 1218 | 1383 | engine mount | 2 |
| 1219 | 1384 | irreversible processes | 2 |
| 1220 | 1385 | descending paths | 1 |
| 1221 | 1386 | dodecagonal sectional | 1 |
| 1222 | 1387 | protection shield | 2 |
| 1223 | 1389 | choked convergent | 3 |
| 1224 | 1390 | full dispersed | 1 |
| 1225 | 1391 | schlieren photographs | 10 |
| 1226 | 1393 | entering irbm | 1 |
| 1227 | 1394 | opposite spin | 1 |
| 1228 | 1395 | walled unstiffened | 1 |
| 1229 | 1396 | hot wire | 10 |
| 1230 | 1398 | disk springs | 1 |
| 1231 | 1399 | teflon shields | 1 |
| 1232 | 1400 | peripheral jets | 1 |
| 1233 | 1402 | sharp cornered | 2 |
| 1234 | 1403 | spiral vortices | 1 |
| 1235 | 1404 | natural frequencies | 7 |
| 1236 | 1405 | pump rotor | 1 |
| 1237 | 1407 | arbitrarily inclined | 1 |
| 1238 | 1408 | specific heats | 18 |
| 1239 | 1409 | rocket motor | 2 |
| 1240 | 1410 | accelerating convergence | 1 |
| 1241 | 1411 | interplanetary orbits | 1 |
| 1242 | 1412 | lingitudinal loads | 1 |
| 1243 | 1413 | variational principle | 3 |
| 1244 | 1414 | lying close | 1 |
| 1245 | 1416 | centrifugal compressors | 2 |
| 1246 | 1417 | blockage corrections | 1 |
| 1247 | 1418 | compressor cascades | 1 |
| 1248 | 1419 | enthalpy potentials | 1 |
| 1249 | 1420 | essential simplicity | 1 |
| 1250 | 1421 | porous coaxial | 1 |
| 1251 | 1422 | full scale | 15 |
| 1252 | 1423 | vehicles traversing | 1 |
| 1253 | 1424 | buckled states | 2 |
| 1254 | 1425 | harmonic oscillations | 3 |
| 1255 | 1426 | acoustic proof | 1 |
| 1256 | 1428 | perfectly conducting | 2 |
| 1257 | 1429 | magnetohydrodynamic duct | 2 |
| 1258 | 1430 | detachment distance | 12 |
| 1259 | 1431 | exhausting rearward | 1 |
| 1260 | 1432 | band width | 2 |
| 1261 | 1433 | interferometric studies | 1 |
| 1262 | 1434 | polar peak | 1 |
| 1263 | 1435 | hinge axis | 2 |
| 1264 | 1436 | sonic boom | 6 |
| 1265 | 1437 | weak shocks | 3 |
| 1266 | 1438 | conservative estimate | 1 |
| 1267 | 1440 | physically reasonable | 2 |
| 1268 | 1441 | eccentricity orbits | 1 |
| 1269 | 1442 | circular cylinderical | 1 |
| 1270 | 1443 | slotted flap | 3 |
| 1271 | 1444 | assumed inaccuracies | 1 |
| 1272 | 1445 | initial imperfections | 8 |
| 1273 | 1446 | fan blade | 1 |
| 1274 | 1447 | satellite observations | 2 |
| 1275 | 1448 | photothermoelastic experiments | 2 |
| 1276 | 1449 | degree dihedral | 1 |
| 1277 | 1450 | considerably smaller | 3 |
| 1278 | 1451 | climb techniques | 1 |
| 1279 | 1452 | virtual work | 2 |
| 1280 | 1454 | hinge moments | 2 |
| 1281 | 1455 | newtonian impact | 6 |
| 1282 | 1456 | eighth order | 2 |
| 1283 | 1457 | virtually constant | 1 |
| 1284 | 1458 | working section | 7 |
| 1285 | 1459 | qualitiative solutions | 1 |
| 1286 | 1460 | indical lift | 2 |
| 1287 | 1461 | modified oseen | 3 |
| 1288 | 1462 | specular type | 1 |
| 1289 | 1463 | shell median | 2 |
| 1290 | 1464 | taylor instability | 1 |
| 1291 | 1465 | surprisingly large | 2 |
| 1292 | 1466 | unit area | 3 |
| 1293 | 1467 | radiation integrals | 1 |
| 1294 | 1468 | gun tunnel | 2 |
| 1295 | 1469 | steady state | 17 |
| 1296 | 1470 | slightly blunted | 4 |
| 1297 | 1471 | symmetrical missiles | 1 |
| 1298 | 1472 | modified newtonian | 11 |
| 1299 | 1473 | molecular dissociation | 1 |
| 1300 | 1474 | diverging nozzle | 1 |
| 1301 | 1475 | weight strength | 5 |
| 1302 | 1476 | sufficiently accurate | 5 |
| 1303 | 1477 | reattached subsonic | 1 |
| 1304 | 1478 | thin pressurised | 1 |
| 1305 | 1479 | cone frustum | 1 |
| 1306 | 1480 | exponential atmosphere | 2 |
| 1307 | 1481 | fluid flowing | 3 |
| 1308 | 1484 | pure torsion | 2 |
| 1309 | 1485 | transverse curvature | 6 |
| 1310 | 1486 | numerical integrations | 3 |
| 1311 | 1487 | bending moments | 6 |
| 1312 | 1488 | taper ratios | 3 |
| 1313 | 1489 | previously reported | 2 |
| 1314 | 1490 | super aerodynamic | 2 |
| 1315 | 1491 | numerically assuming | 1 |
| 1316 | 1492 | drag penalty | 2 |
| 1317 | 1493 | characteristic features | 2 |
| 1318 | 1494 | top conical | 1 |
| 1319 | 1495 | stagnation point | 62 |
| 1320 | 1496 | rigid rotating | 1 |
| 1321 | 1497 | ideal gas | 12 |
| 1322 | 1498 | compressive circumferential | 2 |
| 1323 | 1500 | foot span | 1 |
| 1324 | 1503 | direct gust | 1 |
| 1325 | 1504 | loaded cantilever | 1 |
| 1326 | 1505 | delta wings | 20 |
| 1327 | 1506 | couette type | 2 |
| 1328 | 1507 | insulated flat | 8 |
| 1329 | 1508 | accommodation coefficients | 1 |
| 1330 | 1509 | detailed description | 2 |
| 1331 | 1510 | heat sustaining | 1 |
| 1332 | 1511 | combustible gas | 1 |
| 1333 | 1512 | structure spread | 1 |
| 1334 | 1513 | turbine blade | 3 |
| 1335 | 1514 | coolant material | 1 |
| 1336 | 1515 | unswept wings | 4 |
| 1337 | 1516 | sufficient magnitude | 1 |
| 1338 | 1517 | reaction rate | 4 |
| 1339 | 1518 | jet exhausting | 10 |
| 1340 | 1519 | conic bodies | 1 |
| 1341 | 1521 | free stream | 122 |
| 1342 | 1522 | relaxation phenomena | 1 |
| 1343 | 1523 | numerical examples | 15 |
| 1344 | 1524 | spherical earth | 1 |
| 1345 | 1528 | sir geoffrey | 1 |
| 1346 | 1529 | mm hg | 1 |
| 1347 | 1530 | acoustical signal | 1 |
| 1348 | 1531 | handling qualities | 2 |
| 1349 | 1532 | tailored interface | 1 |
| 1350 | 1533 | euler lagrange | 2 |
| 1351 | 1534 | shielding mechanism | 1 |
| 1352 | 1535 | operating costs | 2 |
| 1353 | 1536 | electron ion | 2 |
| 1354 | 1537 | rae farnborough | 1 |
| 1355 | 1538 | glassy materials | 1 |
| 1356 | 1539 | binary mixture | 4 |
| 1357 | 1540 | sweat cooled | 2 |
| 1358 | 1541 | matric structural | 2 |
| 1359 | 1542 | motor operating | 1 |
| 1360 | 1543 | resonant frequencies | 1 |
| 1361 | 1544 | lie ahead | 1 |
| 1362 | 1546 | simplifying assumptions | 10 |
| 1363 | 1547 | atomic recombination | 1 |
| 1364 | 1548 | solid propellant | 6 |
| 1365 | 1549 | symmetrically loaded | 1 |
| 1366 | 1550 | longitudinal quadrupoles | 1 |
| 1367 | 1551 | chemical reactions | 7 |
| 1368 | 1552 | aileron tab | 1 |
| 1369 | 1553 | propulsion systems | 3 |
| 1370 | 1554 | simultaneous action | 1 |
| 1371 | 1555 | random emission | 1 |
| 1372 | 1556 | joukowski condition | 1 |
| 1373 | 1558 | super satellite | 1 |
| 1374 | 1559 | molecular weight | 3 |
| 1375 | 1560 | probability curves | 1 |
| 1376 | 1561 | uniformly distributed | 10 |
| 1377 | 1563 | vortex cores | 2 |
| 1378 | 1564 | boom intensity | 2 |
| 1379 | 1565 | sandwich construction | 3 |
| 1380 | 1566 | single valued | 1 |
| 1381 | 1568 | moving ripples | 1 |
| 1382 | 1569 | work hardening | 1 |
| 1383 | 1570 | harmonically oscillating | 2 |
| 1384 | 1571 | steady circling | 1 |
| 1385 | 1572 | automatic digital | 2 |
| 1386 | 1573 | detached bow | 3 |
| 1387 | 1574 | landing transport | 1 |
| 1388 | 1575 | compressive hoop | 1 |
| 1389 | 1576 | recovery factors | 6 |
| 1390 | 1577 | uniformly loaded | 6 |
| 1391 | 1578 | initial irregularities | 2 |
| 1392 | 1579 | symmetric joukowsky | 1 |
| 1393 | 1580 | circulatory plane | 1 |
| 1394 | 1581 | elementary considerations | 1 |
| 1395 | 1582 | variational theorem | 2 |
| 1396 | 1583 | polyaxial stress | 1 |
| 1397 | 1584 | acoustic medium | 2 |
| 1398 | 1585 | significantly smaller | 2 |
| 1399 | 1586 | turbine rotor | 1 |
| 1400 | 1588 | fully ionized | 2 |
| 1401 | 1590 | computational procedure | 2 |
| 1402 | 1592 | compressors dash | 1 |
| 1403 | 1594 | facing step | 1 |
| 1404 | 1595 | cross sections | 11 |
| 1405 | 1596 | similarity rule | 3 |
| 1406 | 1597 | caused primarily | 2 |
| 1407 | 1598 | forebody end | 1 |
| 1408 | 1599 | allowable load | 2 |
| 1409 | 1600 | suitable choice | 2 |
| 1410 | 1601 | highly rarefied | 1 |
| 1411 | 1602 | strips cross | 1 |
| 1412 | 1603 | spheric bodies | 1 |
| 1413 | 1604 | major axis | 7 |
| 1414 | 1605 | minimum fuel | 1 |
| 1415 | 1606 | turbine nozzles | 2 |
| 1416 | 1607 | regular shape | 1 |
| 1417 | 1608 | farther downstream | 2 |
| 1418 | 1610 | directly proportional | 1 |
| 1419 | 1611 | streamwise vortices | 1 |
| 1420 | 1612 | line singularities | 1 |
| 1421 | 1613 | accommodation coefficient | 2 |
| 1422 | 1614 | theoretical grounds | 2 |
| 1423 | 1615 | glide vehicle | 2 |
| 1424 | 1616 | paper presents | 21 |
| 1425 | 1617 | lees mixing | 1 |
| 1426 | 1618 | forces acting | 4 |
| 1427 | 1619 | choked wind | 1 |
| 1428 | 1620 | aspect ratio | 52 |
| 1429 | 1621 | curvilinear bodies | 1 |
| 1430 | 1623 | critical heights | 2 |
| 1431 | 1624 | missile motions | 1 |
| 1432 | 1625 | close relationship | 1 |
| 1433 | 1626 | curved sandwich | 2 |
| 1434 | 1627 | plane lattice | 1 |
| 1435 | 1628 | density contours | 2 |
| 1436 | 1629 | streamwise direction | 2 |
| 1437 | 1630 | area rule | 2 |
| 1438 | 1631 | atom mass | 2 |
| 1439 | 1632 | iteration procedure | 2 |
| 1440 | 1633 | cylinder flare | 4 |
| 1441 | 1634 | iterative methods | 2 |
| 1442 | 1635 | spatial distribution | 2 |
| 1443 | 1636 | fixed relative | 1 |
| 1444 | 1637 | viscous dissipation | 5 |
| 1445 | 1638 | takes account | 2 |
| 1446 | 1639 | divergent nozzle | 1 |
| 1447 | 1641 | oscillatory motion | 5 |
| 1448 | 1642 | ground particles | 1 |
| 1449 | 1644 | comparatively small | 3 |
| 1450 | 1645 | gyroscopic effect | 1 |
| 1451 | 1647 | sharp corner | 1 |
| 1452 | 1648 | convenient form | 3 |
| 1453 | 1649 | heating rates | 11 |
| 1454 | 1650 | driver gas | 1 |
| 1455 | 1651 | upper limit | 3 |
| 1456 | 1652 | paper describes | 8 |
| 1457 | 1653 | slot injection | 1 |
| 1458 | 1654 | acoustical problems | 1 |
| 1459 | 1655 | vertical channels | 1 |
| 1460 | 1656 | infinitely conducting | 2 |
| 1461 | 1657 | cutoff mach | 1 |
| 1462 | 1658 | sweptback wings | 5 |
| 1463 | 1659 | exploratory tests | 2 |
| 1464 | 1660 | oval cylindrical | 1 |
| 1465 | 1661 | air bleed | 2 |
| 1466 | 1662 | prolate spheroid | 1 |
| 1467 | 1663 | nautical miles | 1 |
| 1468 | 1664 | carbon dioxide | 4 |
| 1469 | 1665 | human tolerance | 1 |
| 1470 | 1666 | national bureau | 3 |
| 1471 | 1668 | partly wrinkled | 1 |
| 1472 | 1670 | repeated integrals | 2 |
| 1473 | 1671 | splitter vanes | 1 |
| 1474 | 1672 | loose gravel | 2 |
| 1475 | 1673 | flexibly mounted | 2 |
| 1476 | 1675 | composite slabs | 3 |
| 1477 | 1676 | virtual eddy | 1 |
| 1478 | 1677 | parabolic bladed | 1 |
| 1479 | 1678 | digital computers | 1 |
| 1480 | 1679 | simulated turbojet | 2 |
| 1481 | 1682 | joint conductivity | 1 |
| 1482 | 1683 | sounding rocket | 1 |
| 1483 | 1685 | reactive gases | 1 |
| 1484 | 1686 | relative merits | 4 |
| 1485 | 1687 | airframe components | 1 |
| 1486 | 1689 | split flap | 2 |
| 1487 | 1691 | redirecting propeller | 1 |
| 1488 | 1692 | ground launched | 2 |
| 1489 | 1693 | multistage compressor | 3 |
| 1490 | 1694 | unknown twist | 1 |
| 1491 | 1695 | curve slopes | 1 |
| 1492 | 1696 | iterative treatments | 1 |
| 1493 | 1697 | wide variety | 6 |
| 1494 | 1699 | gross weight | 2 |
| 1495 | 1700 | transpiration cooling | 6 |
| 1496 | 1702 | equivalence principle | 1 |
| 1497 | 1703 | hypergeometric functions | 3 |
| 1498 | 1704 | pitching moment | 36 |
| 1499 | 1706 | adjacent stages | 3 |
| 1500 | 1708 | oscillatory derivative | 2 |
| 1501 | 1709 | nonlifting vehicles | 1 |
| 1502 | 1710 | shallow spherical | 4 |
| 1503 | 1711 | neutral curve | 1 |
| 1504 | 1712 | buckle pattern | 2 |
| 1505 | 1713 | initial isovels | 2 |
| 1506 | 1714 | torsional stiffness | 2 |
| 1507 | 1716 | diffusion flame | 2 |
| 1508 | 1717 | geometric variables | 2 |
| 1509 | 1718 | exchange coefficient | 2 |
| 1510 | 1719 | uncambered conical | 1 |
| 1511 | 1720 | wind tunnel | 105 |
| 1512 | 1721 | computing purposes | 2 |
| 1513 | 1722 | perigee distance | 6 |
| 1514 | 1723 | forward movement | 1 |
| 1515 | 1724 | disturbing force | 1 |
| 1516 | 1725 | vibration modes | 4 |
| 1517 | 1726 | immediately downstream | 2 |
| 1518 | 1727 | primary variables | 2 |
| 1519 | 1728 | web plates | 1 |
| 1520 | 1730 | fair agreement | 7 |
| 1521 | 1731 | oscillatory motions | 2 |
| 1522 | 1732 | calculated responses | 2 |
| 1523 | 1733 | nonuniform magnetohydrodynamic | 1 |
| 1524 | 1734 | free molecule | 9 |
| 1525 | 1735 | shallow elastic | 7 |
| 1526 | 1736 | rotating propeller | 1 |
| 1527 | 1737 | flight ballistics | 1 |
| 1528 | 1739 | coordinate transformation | 1 |
| 1529 | 1740 | intermediate enthalpy | 2 |
| 1530 | 1741 | propulsive jet | 5 |
| 1531 | 1742 | peak deceleration | 1 |
| 1532 | 1743 | lighthill formula | 1 |
| 1533 | 1745 | perfect gas | 16 |
| 1534 | 1746 | oscillating airfoils | 3 |
| 1535 | 1747 | asymptotic integration | 3 |
| 1536 | 1748 | graded wall | 1 |
| 1537 | 1749 | compressor performance | 5 |
| 1538 | 1750 | greatly simplified | 2 |
| 1539 | 1751 | practical applications | 5 |
| 1540 | 1752 | convex surfaces | 1 |
| 1541 | 1753 | speed digital | 5 |
| 1542 | 1754 | sufficient accuracy | 3 |
| 1543 | 1755 | compressible fluids | 4 |
| 1544 | 1756 | practical importance | 3 |
| 1545 | 1757 | hypervelocity wind | 2 |
| 1546 | 1758 | graphical form | 3 |
| 1547 | 1759 | lateral extent | 1 |
| 1548 | 1761 | small perturbations | 3 |
| 1549 | 1762 | vtol configurations | 2 |
| 1550 | 1763 | air frame | 3 |
| 1551 | 1764 | gas mixture | 4 |
| 1552 | 1765 | factors governing | 2 |
| 1553 | 1766 | conical disk | 2 |
| 1554 | 1768 | nitrogen dissociation | 2 |
| 1555 | 1769 | spanwise direction | 2 |
| 1556 | 1770 | comparatively simple | 2 |
| 1557 | 1771 | ogive cylinders | 3 |
| 1558 | 1772 | loads surveys | 1 |
| 1559 | 1773 | loading paths | 1 |
| 1560 | 1775 | parallel walls | 3 |
| 1561 | 1777 | classical aerofoil | 1 |
| 1562 | 1778 | circular rings | 1 |
| 1563 | 1779 | dimensional sinking | 3 |
| 1564 | 1780 | galcit hypersonic | 2 |
| 1565 | 1781 | sharp nosed | 4 |
| 1566 | 1782 | united kingdom | 1 |
| 1567 | 1785 | excessive charges | 2 |
| 1568 | 1786 | stewartson illingworth | 1 |
| 1569 | 1788 | ducted fan | 1 |
| 1570 | 1789 | incipient merged | 2 |
| 1571 | 1790 | cowling spinner | 1 |
| 1572 | 1794 | running ripples | 1 |
| 1573 | 1795 | corridor depths | 1 |
| 1574 | 1796 | magneto gasdynamic | 1 |
| 1575 | 1797 | analogues relating | 1 |
| 1576 | 1798 | deep water | 1 |
| 1577 | 1799 | image vortices | 2 |
| 1578 | 1800 | honeycomb sandwich | 2 |
| 1579 | 1801 | schoenherr curve | 1 |
| 1580 | 1802 | conservation laws | 3 |
| 1581 | 1803 | rotating disc | 1 |
| 1582 | 1804 | abrupt stall | 2 |
| 1583 | 1805 | sustained oscillations | 1 |
| 1584 | 1806 | strain accumulation | 1 |
| 1585 | 1807 | winged reentry | 1 |
| 1586 | 1808 | slight blunting | 1 |
| 1587 | 1809 | research laboratories | 2 |
| 1588 | 1810 | propulsion laboratory | 7 |
| 1589 | 1813 | charged particles | 2 |
| 1590 | 1814 | subaudio frequency | 1 |
| 1591 | 1815 | lower bounds | 3 |
| 1592 | 1816 | limit decelerations | 1 |
| 1593 | 1817 | power plants | 1 |
| 1594 | 1818 | fatigue life | 8 |
| 1595 | 1819 | conformal transformation | 3 |
| 1596 | 1820 | semi vertex | 1 |
| 1597 | 1821 | launch vehicle | 1 |
| 1598 | 1822 | ablating material | 3 |
| 1599 | 1823 | moving monatomic | 1 |
| 1600 | 1824 | eddy viscosity | 3 |
| 1601 | 1825 | momentum defect | 2 |
| 1602 | 1827 | conical frustums | 2 |
| 1603 | 1828 | attainable sonic | 1 |
| 1604 | 1829 | rocket motors | 2 |
| 1605 | 1831 | neutral particles | 2 |
| 1606 | 1832 | axially compressed | 4 |
| 1607 | 1833 | quarter chord | 3 |
| 1608 | 1834 | hypervelocity object | 1 |
| 1609 | 1835 | inlet dynamics | 1 |
| 1610 | 1836 | plan forms | 10 |
| 1611 | 1837 | structural members | 3 |
| 1612 | 1838 | chemical reaction | 8 |
| 1613 | 1839 | lateral spread | 1 |
| 1614 | 1840 | liquid metal | 2 |
| 1615 | 1841 | orbit decay | 1 |
| 1616 | 1842 | bessel functions | 2 |
| 1617 | 1843 | subsonic nonplanar | 1 |
| 1618 | 1844 | bluff afterbody | 1 |
| 1619 | 1845 | practice lead | 1 |
| 1620 | 1846 | quarter infinite | 1 |
| 1621 | 1847 | linearly decreasing | 2 |
| 1622 | 1848 | volume constraint | 1 |
| 1623 | 1849 | polar coordinates | 1 |
| 1624 | 1850 | slightly yawing | 1 |
| 1625 | 1851 | skin friction | 72 |
| 1626 | 1852 | column imperfection | 1 |
| 1627 | 1853 | artificial disturbance | 2 |
| 1628 | 1854 | sonic booms | 2 |
| 1629 | 1855 | large sweptwing | 1 |
| 1630 | 1856 | double cascade | 1 |
| 1631 | 1857 | multi stage | 2 |
| 1632 | 1858 | forst order | 1 |
| 1633 | 1859 | coupled chemical | 2 |
| 1634 | 1860 | outward deflection | 1 |
| 1635 | 1861 | downstream movements | 1 |
| 1636 | 1862 | dissociation fraction | 2 |
| 1637 | 1863 | space vehicle | 4 |
| 1638 | 1864 | sharp corners | 1 |
| 1639 | 1865 | joining interaction | 1 |
| 1640 | 1866 | onic aerodynamic | 1 |
| 1641 | 1867 | flat faced | 5 |
| 1642 | 1868 | base annulus | 1 |
| 1643 | 1869 | recent developments | 2 |
| 1644 | 1870 | vehicle developing | 1 |
| 1645 | 1872 | blade erosion | 1 |
| 1646 | 1873 | total head | 5 |
| 1647 | 1874 | translational motion | 2 |
| 1648 | 1875 | coupled mode | 2 |
| 1649 | 1876 | cauchy problem | 2 |
| 1650 | 1878 | concentrated vortices | 2 |
| 1651 | 1879 | matrix formulation | 2 |
| 1652 | 1882 | principal variable | 2 |
| 1653 | 1883 | studying entry | 1 |
| 1654 | 1884 | structural elements | 1 |
| 1655 | 1885 | jet exhausts | 1 |
| 1656 | 1886 | curtain jet | 1 |
| 1657 | 1887 | hyper velocity | 1 |
| 1658 | 1888 | inelastic column | 1 |
| 1659 | 1889 | dissociated combustion | 1 |
| 1660 | 1890 | present day | 2 |
| 1661 | 1891 | time dependent | 12 |
| 1662 | 1892 | fluctuating pressures | 2 |
| 1663 | 1893 | directly applicable | 4 |
| 1664 | 1894 | power law | 8 |
| 1665 | 1896 | wedge airfoils | 1 |
| 1666 | 1897 | scale height | 4 |
| 1667 | 1898 | transient electrical | 2 |
| 1668 | 1899 | wide range | 26 |
| 1669 | 1900 | hall effect | 2 |
| 1670 | 1902 | boattail angle | 2 |
| 1671 | 1903 | incompressible nonviscous | 2 |
| 1672 | 1904 | flap deflection | 3 |
| 1673 | 1905 | trailing vortices | 4 |
| 1674 | 1906 | locally similar | 1 |
| 1675 | 1907 | recombination rates | 3 |
| 1676 | 1908 | elastic core | 3 |
| 1677 | 1909 | discrete noise | 1 |
| 1678 | 1910 | experimental confirmation | 2 |
| 1679 | 1911 | constant property | 3 |
| 1680 | 1912 | conducting fluid | 5 |
| 1681 | 1913 | fundamental interest | 2 |
| 1682 | 1914 | numerical computations | 6 |
| 1683 | 1915 | temperatures ranging | 2 |
| 1684 | 1916 | limit deceleration | 1 |
| 1685 | 1917 | geometrical properties | 2 |
| 1686 | 1918 | experimentally determined | 6 |
| 1687 | 1919 | heating rockets | 1 |
| 1688 | 1922 | sectorial plate | 2 |
| 1689 | 1924 | slip factor | 1 |
| 1690 | 1929 | som reciprocal | 1 |
| 1691 | 1934 | adiabatic index | 2 |
| 1692 | 1935 | cumulative damage | 3 |
| 1693 | 1936 | spectral densities | 1 |
| 1694 | 1937 | strengths exert | 1 |
| 1695 | 1938 | convergent divergent | 9 |
| 1696 | 1939 | pump impeller | 2 |
| 1697 | 1940 | composite slab | 4 |
| 1698 | 1941 | vtol stol | 2 |
| 1699 | 1942 | greatly altered | 2 |
| 1700 | 1943 | secondary injectants | 1 |
| 1701 | 1944 | centrifugal impellers | 2 |
| 1702 | 1946 | imperfect diatomic | 1 |
| 1703 | 1947 | avoid tollmien | 1 |
| 1704 | 1948 | fully submerged | 2 |
| 1705 | 1950 | spherically symmetrical | 2 |
| 1706 | 1951 | cropped delta | 3 |
| 1707 | 1953 | orifice size | 2 |
| 1708 | 1954 | labor involved | 2 |
| 1709 | 1955 | gravel covered | 1 |
| 1710 | 1956 | probable significance | 1 |
| 1711 | 1957 | ballistic missiles | 4 |
| 1712 | 1959 | nitrogen atom | 2 |
| 1713 | 1960 | ignition mechanism | 1 |
| 1714 | 1961 | turbojet engine | 3 |
| 1715 | 1962 | fundamental difficulty | 1 |
| 1716 | 1963 | karman pohlhausen | 9 |
| 1717 | 1964 | supercircular entry | 1 |
| 1718 | 1967 | rigid hoop | 1 |
| 1719 | 1968 | visualization techniques | 1 |
| 1720 | 1969 | horizontal tail | 6 |
| 1721 | 1970 | postbuckling behavior | 5 |
| 1722 | 1971 | chord slotted | 2 |
| 1723 | 1973 | ionization nonequilibrium | 1 |
| 1724 | 1974 | vortex generators | 1 |
| 1725 | 1975 | soft elastic | 3 |
| 1726 | 1976 | core stabilized | 1 |
| 1727 | 1978 | electromagnetic assumptions | 2 |
| 1728 | 1979 | fatigue failures | 2 |
| 1729 | 1980 | cantilever beams | 1 |
| 1730 | 1981 | recovery factor | 6 |
| 1731 | 1982 | standard pitot | 2 |
| 1732 | 1983 | transpiration cooled | 3 |
| 1733 | 1985 | direct tab | 1 |
| 1734 | 1986 | treated separately | 3 |
| 1735 | 1988 | heater performance | 1 |
| 1736 | 1989 | column capacity | 2 |
| 1737 | 1990 | nocturnal flight | 1 |
| 1738 | 1991 | systems governed | 1 |
| 1739 | 1992 | propeller driven | 2 |
| 1740 | 1993 | roughness elements | 5 |
| 1741 | 1994 | similarity laws | 2 |
| 1742 | 1995 | foot hypervelocity | 1 |
| 1743 | 1996 | routine testing | 2 |
| 1744 | 1997 | qualitative description | 3 |
| 1745 | 1998 | vortex sheets | 2 |
| 1746 | 1999 | tapered planform | 1 |
| 1747 | 2000 | narrow delta | 1 |
| 1748 | 2002 | heated cambered | 1 |
| 1749 | 2003 | universal functions | 2 |
| 1750 | 2004 | dimensionless quantities | 2 |
| 1751 | 2005 | tab derivatives | 2 |
| 1752 | 2006 | thermodynamic coupling | 1 |
| 1753 | 2007 | skin stringer | 1 |
| 1754 | 2008 | stable combustion | 1 |
| 1755 | 2009 | drag polars | 1 |
| 1756 | 2010 | spiked nose | 1 |
| 1757 | 2011 | initially straight | 1 |
| 1758 | 2012 | upper ionosphere | 1 |
| 1759 | 2013 | turbine stages | 1 |
| 1760 | 2014 | premature transition | 3 |
| 1761 | 2015 | considerable improvement | 2 |
| 1762 | 2016 | cruising flight | 2 |
| 1763 | 2018 | degree semivertex | 1 |
| 1764 | 2019 | indicial lift | 5 |
| 1765 | 2020 | skin stiffener | 4 |
| 1766 | 2021 | aircraft flying | 4 |
| 1767 | 2022 | resist jet | 1 |
| 1768 | 2023 | tapered swept | 1 |
| 1769 | 2024 | jones slender | 2 |
| 1770 | 2025 | inelastic instability | 1 |
| 1771 | 2026 | propeller vtol | 1 |
| 1772 | 2027 | streamline slope | 2 |
| 1773 | 2028 | pitching motions | 3 |
| 1774 | 2029 | noise sources | 2 |
| 1775 | 2030 | nonequilibrium molecular | 1 |
| 1776 | 2031 | existing theories | 5 |
| 1777 | 2032 | iterative procedure | 3 |
| 1778 | 2033 | finite span | 8 |
| 1779 | 2034 | paper treats | 1 |
| 1780 | 2035 | ogee wings | 1 |
| 1781 | 2036 | ground environment | 1 |
| 1782 | 2037 | pitot tube | 5 |
| 1783 | 2039 | polyatomic gas | 2 |
| 1784 | 2040 | momentum thicknesses | 1 |
| 1785 | 2041 | driven tube | 1 |
| 1786 | 2043 | trends predicted | 2 |
| 1787 | 2044 | distributed suction | 2 |
| 1788 | 2045 | conducting liquid | 1 |
| 1789 | 2046 | center line | 3 |
| 1790 | 2047 | plk method | 1 |
| 1791 | 2048 | practical strengths | 1 |
| 1792 | 2049 | heat fluxes | 2 |
| 1793 | 2050 | including fin | 1 |
| 1794 | 2052 | closely related | 1 |
| 1795 | 2054 | stagnation tank | 1 |
| 1796 | 2055 | modulus load | 1 |
| 1797 | 2056 | median surface | 2 |
| 1798 | 2057 | experimental verification | 5 |
| 1799 | 2058 | nitric oxide | 1 |
| 1800 | 2059 | zoom climb | 1 |
| 1801 | 2060 | entrance flowmeters | 1 |
| 1802 | 2061 | van dyke | 8 |
| 1803 | 2062 | atomic bomb | 1 |
| 1804 | 2064 | bladed impeller | 1 |
| 1805 | 2066 | equally spaced | 2 |
| 1806 | 2067 | hydrocarbon fuel | 1 |
| 1807 | 2068 | converging diverging | 1 |
| 1808 | 2069 | lagrangian thermodynamics | 3 |
| 1809 | 2070 | aluminium alloy | 2 |
| 1810 | 2073 | remained practically | 2 |
| 1811 | 2075 | damage incurred | 1 |
| 1812 | 2076 | suitably chosen | 2 |
| 1813 | 2077 | board stage | 1 |
| 1814 | 2078 | mixture burned | 1 |
| 1815 | 2079 | takes place | 6 |
| 1816 | 2080 | hodographic transformation | 1 |
| 1817 | 2083 | rocket propelled | 2 |
| 1818 | 2084 | additive noise | 1 |
| 1819 | 2085 | highly cooled | 13 |
| 1820 | 2086 | oil smoke | 1 |
| 1821 | 2087 | background source | 1 |
| 1822 | 2088 | rotationally symmetric | 7 |
| 1823 | 2089 | reattaching regions | 1 |
| 1824 | 2091 | square root | 9 |
| 1825 | 2092 | propeller precession | 1 |
| 1826 | 2093 | inch absolute | 1 |
| 1827 | 2094 | sting attached | 2 |
| 1828 | 2095 | axially symmetric | 24 |
| 1829 | 2098 | glancing interaction | 1 |
| 1830 | 2099 | forced oscillation | 1 |
| 1831 | 2101 | exceptional cases | 2 |
| 1832 | 2102 | originally proposed | 2 |
| 1833 | 2103 | midspan section | 1 |
| 1834 | 2104 | vortex sheet | 7 |
| 1835 | 2105 | previous papers | 2 |
| 1836 | 2106 | electrical conductivity | 3 |
| 1837 | 2107 | stiffness derivative | 1 |
| 1838 | 2108 | compatibility condition | 2 |
| 1839 | 2109 | spherical segment | 3 |
| 1840 | 2111 | split trailing | 1 |
| 1841 | 2112 | rheological behavior | 1 |
| 1842 | 2113 | estimates suggest | 1 |
| 1843 | 2114 | chordwise coordinate | 2 |
| 1844 | 2115 | solar radiation | 1 |
| 1845 | 2116 | diatomic gases | 1 |
| 1846 | 2117 | chordwise distortion | 1 |
| 1847 | 2119 | fatigue damage | 2 |
| 1848 | 2120 | qualitative conclusions | 2 |
| 1849 | 2121 | variational principles | 2 |
| 1850 | 2122 | vehicles entering | 2 |
| 1851 | 2123 | axial compression | 23 |
| 1852 | 2124 | detachment distances | 3 |
| 1853 | 2126 | entry corridor | 3 |
| 1854 | 2127 | film cooling | 1 |
| 1855 | 2128 | report presents | 9 |
| 1856 | 2129 | neutral oscillations | 1 |
| 1857 | 2131 | trip required | 1 |
| 1858 | 2132 | nonstationary flows | 1 |
| 1859 | 2133 | twist distributions | 3 |
| 1860 | 2134 | nonporous wall | 1 |
| 1861 | 2135 | radiative heating | 2 |
| 1862 | 2136 | cross section | 28 |
| 1863 | 2137 | inelastic behaviour | 1 |
| 1864 | 2138 | purely elastic | 1 |
| 1865 | 2139 | impingement problem | 1 |
| 1866 | 2140 | solved analytically | 2 |
| 1867 | 2142 | trailing edge | 22 |
| 1868 | 2143 | parallel planes | 2 |
| 1869 | 2144 | tail fins | 2 |
| 1870 | 2145 | boattail angles | 1 |
| 1871 | 2146 | frequency spectra | 1 |
| 1872 | 2147 | linear algebraic | 2 |
| 1873 | 2148 | comparative tests | 1 |
| 1874 | 2149 | downstream distances | 3 |
| 1875 | 2150 | span loadings | 2 |
| 1876 | 2151 | round nosed | 2 |
| 1877 | 2152 | foreign gases | 1 |
| 1878 | 2153 | nozzle beneath | 2 |
| 1879 | 2155 | spanwise flexible | 1 |
| 1880 | 2157 | weak disturbances | 1 |
| 1881 | 2158 | instantaneous elastic | 1 |
| 1882 | 2159 | transport airplane | 1 |
| 1883 | 2160 | negative slope | 2 |
| 1884 | 2161 | disturbance reflected | 1 |
| 1885 | 2163 | inch diameter | 3 |
| 1886 | 2164 | mass fraction | 1 |
| 1887 | 2165 | axial symmetry | 7 |
| 1888 | 2166 | complete description | 3 |
| 1889 | 2167 | circular hole | 1 |
| 1890 | 2168 | spacecraft lift | 1 |
| 1891 | 2169 | trimmed lift | 2 |
| 1892 | 2170 | direction perpendicular | 2 |
| 1893 | 2172 | meridional bending | 1 |
| 1894 | 2174 | trajectory calculations | 2 |
| 1895 | 2175 | single wedge | 3 |
| 1896 | 2177 | previous work | 6 |
| 1897 | 2178 | constant lies | 2 |
| 1898 | 2179 | cone semivertex | 1 |
| 1899 | 2180 | frequency band | 2 |
| 1900 | 2181 | increased effectiveness | 1 |
| 1901 | 2182 | gust frequency | 1 |
| 1902 | 2183 | crossflow plane | 2 |
| 1903 | 2184 | inviscid rotational | 3 |
| 1904 | 2185 | temperature alloys | 2 |
| 1905 | 2186 | cambered rectangular | 1 |
| 1906 | 2187 | cruciform configuration | 1 |
| 1907 | 2188 | gust forces | 1 |
| 1908 | 2190 | effect machines | 3 |