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Tested code on queries with multiple phrases

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1 what similarity laws must be obeyed when constructing aeroelastic models of heated high speed aircraft .
3 what problems of heat conduction in composite slabs have been solved so far .
4 can a criterion be developed to show empirically the validity of flow solutions for chemically reacting gas mixtures based on the simplifying assumption of instantaneous local chemical equilibrium .
5 what chemical kinetic system is applicable to hypersonic aerodynamic problems .
10 are real-gas transport properties for air available over a wide range of enthalpies and densities .
11 is it possible to find an analytical, similar solution of the strong blast wave problem in the newtonian approximation .
20 has anyone formally determined the influence of joule heating, produced by the induced current, in magnetohydrodynamic free convection flows under general conditions .
25 does a practical flow follow the theoretical concepts for the interaction between adjacent blade rows of a supersonic cascade .
29 what is the effect of cross sectional shape on the flow over simple delta wings with sharp leading edges .
47 what are the existing solutions for hypersonic viscous interactions over an insulated flat plate .
53 what investigations have been made of the flow field about a body moving through a rarefied, partially ionized gas in the presence of a magnetic field .
58 is it possible to determine rates of forced convective heat transfer from heated cylinders of non-circular cross-section, (the fluid flow being along the generators) .
74 how significant is the possible pressure of a dissociated free stream with respect to the realization of hypersonic simulation in high enthalpy wind tunnels .
86 can a satisfactory experimental technique be developed for measuring oscillatory derivatives on slender sting-mounted models in supersonic wind tunnels .
88 how does a satellite orbit contract under the action of air drag in an atmosphere in which the scale height varies with altitude .
89 how is the flow at transonic speeds about a delta wing different from that on a closely-related tapered sweptback wing .
92 given complete freedom in the design of an airplane, what procedure would be used in order to minimize sonic boom intensity, and is there a limit to the degree of minimizing that can be accomplished .
94 what is the theoretical heat transfer rate at the stagnation point of a blunt body .
100 what are the effects of initial imperfections on the elastic buckling of cylindrical shells under axial compression .
105 what is the effect of an internal liquid column on the breathing vibrations of a cylindrical shell .
120 are previous analyses of circumferential thermal buckling of circular cylindrical shells unnecessarily involved or even inaccurate due to the assumed forms of buckling mode .
128 has anyone programmed a pump design method for a high-speed digital computer .
137 have any analytical studies been conducted on the time-to-failure mechanism associated with creep collapse for a long circular cylindrical shell which exhibits both primary and secondary creep as well as elastic deformations under various distributed force systems .
138 has the effect of initial stresses, on the frequencies of vibration of circular cylindrical shells, been investigated .
139 has the effect of the change of initial pressure due to deformation, on the frequencies of vibration of circular cylindrical shells been investigated .
147 what are the equations which define the stability of simply supported corrugated core sandwich cylinders .
157 have flow fields been calculated for blunt-nosed bodies and compared with experiment for a wide range of free stream conditions and body shapes .
159 what is the magnitude of aerodynamic damping in flexible vibration modes of a slender body of revolution characteristic of launch vehicles .
161 is there an integral method to give a single and sufficiently accurate method of calculating the laminar separate point for various incompressible and compressible boundary layers with zero heat transfer .
182 effects of leading-edge bluntness on the flutter characteristics of some square-planform double-wedge airfoils at mach numbers less than 15.4.
187 has anyone analytically or experimentally investigated the effects of internal pressure on the buckling of circular-cylindrical shells under bending .
198 is there any information available on the difference in the effects of various edge conditions on the buckling of cylindrical shells .
200 are asymptotic methods sufficiently accurate in the determination of pre-buckling stresses in torispherical shells, or must we resort to numerical methods .
210 has anyone analytically investigated the stabilizing influence of soft elastic cores on the buckling strength of cylindrical shells subjected to non-uniform external pressure .
211 what papers are available on the buckling of empty cylindrical shells under non-uniform pressure .
212 what effect do thermal stresses have on the compressive buckling strength of ring-stiffened cylinders .
1 1 what similarity laws must be obeyed when constructing aeroelastic models of heated high speed aircraft .
2 3 what problems of heat conduction in composite slabs have been solved so far .
3 4 can a criterion be developed to show empirically the validity of flow solutions for chemically reacting gas mixtures based on the simplifying assumption of instantaneous local chemical equilibrium .
4 5 what chemical kinetic system is applicable to hypersonic aerodynamic problems .
5 10 are real-gas transport properties for air available over a wide range of enthalpies and densities .
6 11 is it possible to find an analytical, similar solution of the strong blast wave problem in the newtonian approximation .
7 20 has anyone formally determined the influence of joule heating, produced by the induced current, in magnetohydrodynamic free convection flows under general conditions .
8 25 does a practical flow follow the theoretical concepts for the interaction between adjacent blade rows of a supersonic cascade .
9 29 what is the effect of cross sectional shape on the flow over simple delta wings with sharp leading edges .
10 47 what are the existing solutions for hypersonic viscous interactions over an insulated flat plate .
11 53 what investigations have been made of the flow field about a body moving through a rarefied, partially ionized gas in the presence of a magnetic field .
12 58 is it possible to determine rates of forced convective heat transfer from heated cylinders of non-circular cross-section, (the fluid flow being along the generators) .
13 74 how significant is the possible pressure of a dissociated free stream with respect to the realization of hypersonic simulation in high enthalpy wind tunnels .
14 86 can a satisfactory experimental technique be developed for measuring oscillatory derivatives on slender sting-mounted models in supersonic wind tunnels .
15 88 how does a satellite orbit contract under the action of air drag in an atmosphere in which the scale height varies with altitude .
16 89 how is the flow at transonic speeds about a delta wing different from that on a closely-related tapered sweptback wing .
17 92 given complete freedom in the design of an airplane, what procedure would be used in order to minimize sonic boom intensity, and is there a limit to the degree of minimizing that can be accomplished .
18 94 what is the theoretical heat transfer rate at the stagnation point of a blunt body .
19 100 what are the effects of initial imperfections on the elastic buckling of cylindrical shells under axial compression .
20 105 what is the effect of an internal liquid column on the breathing vibrations of a cylindrical shell .
21 120 are previous analyses of circumferential thermal buckling of circular cylindrical shells unnecessarily involved or even inaccurate due to the assumed forms of buckling mode .
22 128 has anyone programmed a pump design method for a high-speed digital computer .
23 137 have any analytical studies been conducted on the time-to-failure mechanism associated with creep collapse for a long circular cylindrical shell which exhibits both primary and secondary creep as well as elastic deformations under various distributed force systems .
24 138 has the effect of initial stresses, on the frequencies of vibration of circular cylindrical shells, been investigated .
25 139 has the effect of the change of initial pressure due to deformation, on the frequencies of vibration of circular cylindrical shells been investigated .
26 147 what are the equations which define the stability of simply supported corrugated core sandwich cylinders .
27 157 have flow fields been calculated for blunt-nosed bodies and compared with experiment for a wide range of free stream conditions and body shapes .
28 159 what is the magnitude of aerodynamic damping in flexible vibration modes of a slender body of revolution characteristic of launch vehicles .
29 161 is there an integral method to give a single and sufficiently accurate method of calculating the laminar separate point for various incompressible and compressible boundary layers with zero heat transfer .
30 182 effects of leading-edge bluntness on the flutter characteristics of some square-planform double-wedge airfoils at mach numbers less than 15.4.
31 187 has anyone analytically or experimentally investigated the effects of internal pressure on the buckling of circular-cylindrical shells under bending .
32 198 is there any information available on the difference in the effects of various edge conditions on the buckling of cylindrical shells .
33 200 are asymptotic methods sufficiently accurate in the determination of pre-buckling stresses in torispherical shells, or must we resort to numerical methods .
34 210 has anyone analytically investigated the stabilizing influence of soft elastic cores on the buckling strength of cylindrical shells subjected to non-uniform external pressure .
35 211 what papers are available on the buckling of empty cylindrical shells under non-uniform pressure .
36 212 what effect do thermal stresses have on the compressive buckling strength of ring-stiffened cylinders .