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STABILITY AND CONTROL CHARACTERISTICS AT A MACH NUMBER OF 2.01 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGSStability and control of supersonic vtol airplane model having broad fuselage and small delta wing
Document ID
19630006264
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Driver, C. (NASA Langley Research Center Hampton, VA, United States)
Spearman, M. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1961
Subject Category
Biosciences
Report/Patent Number
NASA-TM-X-441
Report Number: NASA-TM-X-441
Accession Number
63N16140
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
STABILITY AND CONTROL
FUSELAGE
DELTA WING
VTOL AIRCRAFT

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