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Additional experiments with flat-top wing- body combinations at high supersonic speedsFlat top wing body configuration effects on aerodynamic characteristics of supersonic aircraft
Document ID
19660024022
Acquisition Source
Legacy CDMS
Document Type
Other - NACA Research Memorandum
Authors
Gloria, H. R. (NASA Ames Research Center Moffett Field, CA, United States)
Syvertson, C. A. (NASA Ames Research Center Moffett Field, CA, United States)
Wong, T. J. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
February 19, 1957
Subject Category
Aerodynamics
Report/Patent Number
NACA-RM-A56111
Accession Number
66N33312
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
AERODYNAMIC CHARACTERISTICS
SUPERSONIC AIRCRAFT
WING BODY
AIRCRAFT DESIGN

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