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High-subsonic-speed investigation of the static longitudinal aerodynamic characteristics of several delta-wing configurations for angles of attack from 0 deg to 90 degHigh subsonic speed of static longitudinal aerodynamic characteristics of delta wing configuration for angle of attack from 0 deg to 90 deg
Document ID
19650003093
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Spencer, B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
December 1, 1959
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-168
Accession Number
65N12694
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
SUBSONIC SPEED
STATIC AERODYNAMIC CHARACTERISTICS

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