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EFFECT OF VERTICAL-TAIL MODIFICATIONS ON THE STATIC STABILITY CHARACTERISTICS AT A MACH NUMBER OF 2.2 OF A SUPERSONIC VTOL AIRPLANE MODEL HAVING A BROAD FUSELAGE AND SMALL DELTA WINGSEffect of vertical tail modifications on static stability of vtol supersonic aircraft
Document ID
19630007289
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Robinson, R. B. (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
April 1, 1961
Subject Category
Biosciences
Report/Patent Number
NASA-TM-X-519
Report Number: NASA-TM-X-519
Accession Number
63N17165
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
SUPERSONIC AIRCRAFT
VERTICAL TAIL
VTOL AIRCRAFT
STATIC STABILITY

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