Stability and Controls Analysis and Flight Test Results of a 24-Foot Telescoping Nose Boom on an F-15B Airplane
Stability and Controls Analysis and Flight Test Results of a 24-Foot Telescoping Nose Boom on an F-15B Airplane
- Neue Suche nach: Moua, Cheng M.
- Neue Suche nach: Cox, Timothy H.
- Neue Suche nach: McWherter, Shaun C.
- Neue Suche nach: Moua, Cheng M.
- Neue Suche nach: Cox, Timothy H.
- Neue Suche nach: McWherter, Shaun C.
The Quiet Spike(TradeMark) F-15B flight research program investigated supersonic shock reduction using a 24-ft telescoping nose boom on an F-15B airplane. The program goal was to collect flight data for model validation up to 1.8 Mach. In the area of stability and controls, the primary concerns were to assess the potential destabilizing effect of the oversized nose boom on the stability, controllability, and handling qualities of the airplane and to ensure adequate stability margins across the entire research flight envelope. This paper reports on the stability and control analytical methods, flight envelope clearance approach, and flight test results of the F-15B telescoping nose boom configuration. Also discussed are brief pilot commentary on typical piloting tasks and refueling tasks.
Dokumentinformationen
Stability and Controls Analysis and Flight Test Results of a 24-Foot Telescoping Nose Boom on an F-15B Airplane
AIAA Aerospace Sciences Meeting and Exhibit ; 2008 ; Reno, NV, United States
2008-01-07
Aufsatz (Konferenz)
Keine Angabe
Englisch
Ähnliche Titel
Stability and Controls Flight Test Results of a 24ft Telescoping Nose Boom on an F-15B Aircraft
| British Library Conference Proceedings | 2008