Subsonic and transonic dynamic stability characteristics of the space shuttle launch vehicle

An investigation has been conducted to determine the subsonic and transonic dynamic stability characteristics of a 0.015 scale model of the space shuttle launch vehicle. These tests were conducted in the Langley 8-foot transonic pressure tunnel over a Mach number range from 0.3 to 1.2. Forced oscill...

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Bibliographische Detailangaben

Hauptverfasser:	Freeman, D. C., Jr, Boyden, R. P., Davenport, E. E.
Format:	Report
Sprache:	eng
Schlagworte:	Aeronautics (General)
Online-Zugang:	Volltext bestellen
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