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V/stol handling qualities as determined by flight test and simulation techniques.
Bell X-14A test vehicle used to determine control power and damping requirements for V/STOL AIRCRAFT
Document ID
19650032844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Drinkwater, F. J., III
Quigley, H. C.
Rolls, L. S.
Turner, H. L.
Date Acquired
August 2, 2013
Publication Date
January 1, 1964
Subject Category
Aircraft
Accession Number
65A15548
Distribution Limits
Public
Copyright
Other
Keywords
FLIGHT STABILITY TEST
FLIGHT TEST
AIRCRAFT STABILITY
X-14 AIRCRAFT
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