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Transonic Wind-tunnel Investigation of Static Longitudinal and Lateral Stability and Control Characteristics and Drag Rise of a Representative Fighter AirplaneTransonic wind tunnel study of static longitudinal and lateral stability and control characteristics and drag rise of fighter aircraft
Document ID
19660024792
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Memorandum (MEMO)
Authors
Pierpont, P. K. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1959
Subject Category
Aircraft
Report/Patent Number
NASA-MEMO-12-14-58L
Report Number: NASA-MEMO-12-14-58L
Accession Number
66N34082
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STATIC STABILITY AND CONTROL
DRAG
LATERAL STABILITY AND CONTROL
TRANSONIC WIND TUNNEL
FIGHTER AIRCRAFT
LONGITUDINAL STABILITY AND CONTROL

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