|
NAS 1.12/7:D-15811
|
Exploration Technology Program : accomplishments and technology infusion / |
1 |
|
NAS 1.12:8
|
Mass transfer cooling near the stagnation point / |
1 |
|
NAS 1.12/8:46
|
Viking-Mars : anatomy of success / |
1 |
|
NAS 1.12:9
|
A Theoretical study of stagnation-point ablation / |
1 |
|
NAS 1.12:10
|
Stagnation-point shielding by melting and vaporization / |
1 |
|
NAS 1.12/10:
|
Welcome to the planets. |
1 |
|
NAS 1.12:11
|
An approximate analytical method for studying entry into planetary atmospheres / |
1 |
|
NAS 1.12:12
|
Effect of the proximity of the wing first-bending frequency and the short-period frequency on the airplane dynamic-response factor / |
1 |
|
NAS 1.12:13
|
Effect of a stringer on the stress concentration due to a crack in a thin sheet / |
1 |
|
NAS 1.12:14
|
A method for calculation of hydrodynamic lift for submerged and planing rectangular lifting surfaces / |
1 |
|
NAS 1.12:15
|
Approximate analytical solutions for hypersonic flow over slender power law bodies / |
1 |
|
NAS 1.12:16
|
Effects of mach number and wall-temperature ratio on turbulent heat transfer at mach numbers from 3 to 5 / |
1 |
|
NAS 1.12:17
|
Analysis of turbulent flow and heat transfer on a flat plate at high Mach numbers with variable fluid properties / |
1 |
|
NAS 1.12:18
|
Several methods for aerodynamic reduction of static-pressure sensing errors for aircraft at subsonic, near-sonic, and low supersonic speeds / |
1 |
|
NAS 1.12:19
|
Theoretical analysis of the longitudinal behavior of an automatically controlled supersonic interceptor during the attack phase / |
1 |
|
NAS 1.12:20
|
Tire-to-surface friction-coefficient measurements with a C-123B airplane on various runway surfaces / |
1 |
|
NAS 1.12:21
|
On solutions for the transient response of beams / |
1 |
|
NAS 1.12:22
|
Boundary-layer displacement effects in air at mach numbers of 6.8 and 9.6 / |
1 |
|
NAS 1.12:23
|
Effect of surface roughness on characteristics of spherical shock waves / |
1 |
|
NAS 1.12:24
|
An improved first-approximation theory for thin shells / |
1 |
