Call Number (LC) Title Results
NAS 1.15:100427 Development of an integrated set of research facilities for the support of research flight test 1
NAS 1.15:100428 Development of a mobile research flight rest support capability 1
NAS 1.15:100429 Development of an interactive real-time graphics system for the display of vehicle space positioning 1
NAS 1.15:100430 Formulation of a general technique for predicting pneumatic attenuation errors in airborne pressure sensing devices 1
NAS 1.15:100431 Performance improvements of an F-15 airplane with an integrated engine-flight control system 1
NAS 1.15:100432 Development of a real-time aeroperformance analysis technique for the X-29A advanced technology demonstrator 1
NAS 1.15:100433 Flight tests of external modifications used to reduce blunt base drag 1
NAS 1.15:100434 Operational viewpoint of the X-29A digital flight control system 1
NAS 1.15:100435 The Use of an automated flight test management system in the development of a rapid prototyping flight research facility 1
NAS 1.15:100436 Surface flow visualization of separated flows on the forebody of an F-18 aircraft and wind-tunnel model 1
NAS 1.15:100437 Configuration management issues and objectives for a real-time research flight test support facility 1
NAS 1.15:100438 In-flight rain damage tests of the shuttle thermal protection system 1
NAS 1.15:100439 Flight research and testing 1
NAS 1.15:100440 Constructing "gloved" wings for aerodynamic studies 1
NAS 1.15:100442 Application of flight systems methodologies to the validation of knowledge-based systems 1
NAS 1.15:100443 Measured and predicted pressure distributions on the AFTI/F-111 mission adaptive wing 1
NAS 1.15:100444 Techniques used in the F-14 variable-sweep transition flight experiment 1
NAS 1.15:100445 Current flight test experience related to structural divergence of forward-swept wings 1
NAS 1.15:100446 The effects of excitation waveforms and shaker moving mass on the measured modal characteristics of a 2- by 5-foot aluminum plate 1
NAS 1.15:100448 Ground vibration test results of a JetStar airplane using impulsive sine excitation 1