NAS 1.26:2695
|
Calculation of subsonic and supersonic steady and unsteady aerodynamic forces using velocity potential aerodynamic elements / |
1 |
NAS 1.26:2696
|
Reflection-plane tests of spoilers on an advanced technology wing with a large Fowler flap / |
1 |
NAS 1.26:2697
|
Development of an improved coating for polybenzimidazole foam / |
1 |
NAS 1.26:2698
|
Finite element computer program to analyze cracked orthotropic sheets / |
1 |
NAS 1.26:2699
|
An exploratory study to determine the integrated technological air transportation system ground requirements of liquid-hydrogen-fueled subsonic, long-haul civil air transports / |
1 |
NAS 1.26:2700
|
LH2 Airport requirements study / |
1 |
NAS 1.26:2701
|
Effects of motion on jet exhaust noise from aircraft / |
1 |
NAS 1.26:2702
|
Effects of forward velocity on turbulent jet mixing noise / |
1 |
NAS 1.26:2703
|
Experimental study of transient dynamics of a flexible rotor / |
1 |
NAS 1.26:2704
|
Combustion contribution to noise in jet engines / |
1 |
NAS 1.26:2705
|
Calculation of the longitudinal aerodynamics characteristics of wing-flap configurations with externally blown flaps / |
1 |
NAS 1.26:2706
|
A computer program to calculate the longitudinal aerodynamic characteristics of wing-flap configurations with extremely blown flaps / |
1 |
NAS 1.26:2707
|
Space shuttle electromagnetic environment experiment phase A; Definition study / |
1 |
NAS 1.26:2708
|
Noise suppression with high Mach number inlets / |
1 |
NAS 1.26:2709
|
Industry workshop on large space structures, executive summary / |
1 |
NAS 1.26:2710
|
In-flight simulation study of decoupled longitudinal controls for the approach and landing of a STOL aircraft / |
1 |
NAS 1.26:2711/
|
Carbide coated fibers in graphite-aluminum composites : progress report / |
1 |
NAS 1.26:2712
|
The electron Boltzmann equation in a plasma generated by fission fragments / |
1 |
NAS 1.26:2713
|
Hover performance tests of full scale variable geometry rotors / |
1 |
NAS 1.26:2714
|
Landing gear and cavity noise prediction / |
1 |