| Call Number (LC) | Title | Results |
|---|---|---|
| NAS 1.15:104275 | Aircraft ground vibration testing at the NASA Dryden Flight Research Facility, 1993 | 1 |
| NAS 1.15:104276 | Water tunnel flow visualization study of a 4.4% scale X-31 forebody | 1 |
| NAS 1.15:104277 | Effects of mass on aircraft sidearm controller characteristics | 1 |
| NAS 1.15:104278 | An electronic workshop on the performance seeking control and propulsion controlled aircraft results of the F-15 Highly Integrated Digital Electronic Control Flight Research Program proceedings of the electronic workshop / | 1 |
| NAS 1.15:104307 | Preliminary airborne measurements for the SR-71 sonic boom propagation experiment | 1 |
| NAS 1.15:104308 |
A flying qualities study of longitudinal long-term dynamics of hypersonic planes A flying qualities study of longitudinal long-term dynamics of hypersonic planes / |
2 |
| NAS 1.15:104309 |
A conversion of wheatstone bridge to current-loop signal conditioning for strain gages A conversion of Wheatstone bridge to current-loop signal conditioning for strain gages / |
2 |
| NAS 1.15:104310 | Ground-based sensors for the SR-71 sonic boom propagation experiment | 1 |
| NAS 1.15:104312 | Ground-recorded sonic boom signatures of F-18 aircraft in formation flight | 1 |
| NAS 1.15:104313 | A comparison of hypersonic vehicle flight and prediction results | 1 |
| NAS 1.15:104314 | In-flight demonstration of a Real-Time Flush Airdata Sensing (RT-FADS) system | 1 |
| NAS 1.15:104315 | Flight simulation software at NASA Dryden Flight Research Center | 1 |
| NAS 1.15:104316 |
Airdata measurement and calibration / Airdata measurement and calibration |
2 |
| NAS 1.15:104318 |
Coherent lidar turbulence measurement for gust load alleviation / Coherent lidar turbulence measurement for gust load alleviation |
2 |
| NAS 1.15:104322 |
Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers / Evaluation of high-angle-of-attack handling qualities for the X-31A using standard evaluation maneuvers |
2 |
| NAS 1.15:104324 |
Design and integration of an actuated nose strake control system Design and integration of an actuated nose strake control system / |
2 |
| NAS 1.15:104326 |
[Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests] Flight and static exhaust flow properties of an F110-GE-129 engine in an F-16XL airplane during acoustic tests / |
2 |
| NAS 1.15:104327 |
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack contract NAS 3-26617 / F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack / |
2 |
| NAS 1.15:104328 | An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft | 1 |
| NAS 1.15:104329 |
Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60̊ angle of attack contract NAS 3-26617 / Inlet distortion for an F/A-18A aircraft during steady aerodynamic conditions up to 60 ° angle of attack / |
2 |
