Zoekeend-Phrase-Indexing/ngrams.csv

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