Call Number (LC) Title Results
NAS 1.15:104273 Thermal-fluid analysis of the fill and drain operations of a cryogenic fuel tank 1
NAS 1.15:104274 Strain gage measurement errors in the transient heating of structural components 1
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 /
F/A-18A inlet flow characteristics during maneuvers with rapidly changing angle of attack contract NAS 3-26617 / 		2