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THE EFFECTS OF WING PLAN FORM ON THE STATIC LONGITUDINAL AERODYNAMIC CHARACTERISTICS OF A FLAT-TOP HYPERSONIC AIRCRAFT AT MACH NUMBERS FROM 0.6 TO 1.4Wing planform effect on static longitudinal aerodynamic characteristics of flat top hypersonic aircraft at transonic speeds
Document ID
19630006262
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Treon, S. L. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1960
Subject Category
Biosciences
Report/Patent Number
NASA-TM-X-364
Accession Number
63N16138
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
HYPERSONIC AIRCRAFT
LONGITUDINAL STABILITY
AERODYNAMIC CHARACTERISTICS
WING PLANFORM
TRANSONIC SPEED

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