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Effects of wing height on the stability and control characteristics at a mach number of 2.01 of a canard airplane configuration with a 70 deg delta wingWing height effect on stability and control of 70 deg delta-wing canard-aircraft configuration at Mach 2.01
Document ID
19650003199
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, 1960
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-328
Report Number: NASA-TM-X-328
Accession Number
65N12800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
DELTA WING
CANARD
STABILITY AND CONTROL
AIRCRAFT CONFIGURATION

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