NAS 1.15:109154
|
Potential impacts of advanced aerodynamic technology on air transportation system productivity |
1 |
NAS 1.15:109156
|
Dynamic stability instrumentation system (DSIS) |
1 |
NAS 1.15:109157
|
16-foot transonic tunnel test section flowfield survey |
1 |
NAS 1.15:109158
|
Why do airlines want and use thrust reversers? a compilation of airline industry responses to a survey regarding the use of thrust reversers on commercial transport planes / |
1 |
NAS 1.15:109159
|
Summary of OARE flight calibration measurements |
1 |
NAS 1.15:109160
|
Dynamic stability instrumentation system (DSIS) |
1 |
NAS 1.15:109161
|
Compendium of NASA data base for the global tropospheric experiment's arctic boundary layer experiments ABLE-3A and ABLE-3B |
1 |
NAS 1.15:109162
|
World wide web implementation of the Langley technical report server |
1 |
NAS 1.15:109163
|
A review of 50 years of aerodynamic research with NACA/NASA |
1 |
NAS 1.15:109164
|
NASA/DoD aerospace knowledge diffusion research project. |
1 |
NAS 1.15:109165
|
Aviation system capacity improvements through technology |
1 |
NAS 1.15:109166
|
Mathematical modeling of a class of multibody flexible space structures |
1 |
NAS 1.15:109168
|
Flutter clearance flight tests of an OV-10A airplane modified for wake vortex flight experiments |
1 |
NAS 1.15:109169
|
NASA/DoD aerospace knowledge diffusion research project. results of the phase 1 SME mail survey / |
1 |
NAS 1.15:109171
|
A crew-centered flight deck design philosophy for high-speed civil transport (HSCT) aircraft |
1 |
NAS 1.15:109172
|
A strategy for electronic dissemination of NASA Langley technical publications |
1 |
NAS 1.15:109173
|
Grid resolution and solution convergence for Mars pathfinder forebody |
1 |
NAS 1.15:109174
|
The personal aircraft status and issues / |
1 |
NAS 1.15:109175
|
Design and evaluation of a foam-filled hat-stiffened panel concept for aircraft primary structural applications |
1 |
NAS 1.15:109176
|
An optimized implementation of a fault-tolerant clock synchronization circuit |
1 |