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Supersonic aerodynamic characteristics of triangular plan-form models at angles of attack to 90 degreesAerodynamic characteristics of triangular planform wing models at supersonic speeds
Document ID
19660024034
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Kaattari, G. E. (NASA Ames Research Center Moffett Field, CA, United States)
Wiggins, L. E. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1961
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-568
Accession Number
66N33324
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PLANFORM
AERODYNAMIC CHARACTERISTICS
SUPERSONIC SPEED
TRIANGULAR WING

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