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Effect of Forebody Strakes on the Aerodynamic Characteristics in Pitch and Sideslip of a Hypersonic Airplane Configuration at Mach Numbers of 1.41, 2.01, and 6.86Effect of forebody strakes on aerodynamic characteristics in sideslip and pitch of hypersonic aircraft configurations
Document ID
19650018848
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Driver, C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-116
Report Number: NASA-TM-X-116
Accession Number
65N28449
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
PITCH ATTITUDE
FOREBODY
SIDESLIP
HYPERSONIC AIRCRAFT
AERODYNAMIC CHARACTERISTICS

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