NAS 1.12:72
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A Supersonic area rule and an application to the design of a wing-body combination with high lift-drag ratios / |
1 |
NAS 1.12:73
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A study of the simulation of flow with free-stream Mach number 1 in a choked wind tunnel / |
1 |
NAS 1.12:74
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The Lateral response of airplanes to random atmospheric turbulence / |
1 |
NAS 1.12:75
|
Analytical study of soft landings on gas-filled bags / |
1 |
NAS 1.12:76
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Calculated effects of body shape on the bow-shock overpressures in the far field of bodies in supersonic flow / |
1 |
NAS 1.12:77
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Flow in the base region of axisymmetric and two-dimensional configurations / |
1 |
NAS 1.12:78
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Analytic study of induced pressure on long bodies of revolution with varying nose bluntness at hypersonic speeds / |
1 |
NAS 1.12:79
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Fast interplanetary missions with low-thrust propulsion systems / |
1 |
NAS 1.12:80
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The Effect of lift on entry corridor depth and guidance requirements for the return lunar flight / |
1 |
NAS 1.12:81
|
Alignment charts for transport properties, viscosity, thermal conductivity, and diffusion coefficients for nonpolar gases and gas mixtures at low density / |
1 |
NAS 1.12:82
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Turbulent skin friction at high Mach numbers and Reynolds numbers in air and helium / |
1 |
NAS 1.12:83
|
A theoretical study of the angular motions of spinning bodies in space / |
1 |
NAS 1.12:84
|
Ordinates and theoretical pressure-distribution data for NACA 6- and 6A-series airfoil sections with thicknesses from 2 to 21 and from 2 to 15 percent chord, respectively / |
1 |
NAS 1.12:85
|
A nonlinear theory for predicting the effects of unsteady laminar, turbulent, or transitional boundary layers on the attenuation of shock waves in a shock tube with experimental comparison / |
1 |
NAS 1.12:86
|
The drag coefficient of parabolic bodies of revolution operating at zero cavitation number and zero angle of yaw / |
1 |
NAS 1.12:87
|
A study of the positions and velocities of a space station and a ferry vehicle during rendezvous and return / |
1 |
NAS 1.12:88
|
Theoretical pressure distributions on wings of finite span at zero incidence for mach numbers near 1 / |
1 |
NAS 1.12:89
|
Trajectory control for vehicles entering the earth's atmosphere at small flight-path angles / |
1 |
NAS 1.12:90
|
Theory and apparatus for measurement of emissivity for radiative cooling of hypersonic aircraft with data for inconel, inconel X, stainless steel 303, and titanium alloy RS-120 / |
1 |
NAS 1.12:91
|
The effect of repeated stressing on the behavior of lithium fluoride crystals / |
1 |