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Experimental and analytical investigations to improve low-speed performance and stability and control characteristics of supersonic cruise fighter vehiclesSmall- and large-scale models of supersonic cruise fighter vehicles were used to determine the effectiveness of airframe/propulsion integration concepts for improved low-speed performance and stability and control characteristics. Computer programs were used for engine/airframe sizing studies to yield optimum vehicle performance.
Document ID
19770021192
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Graham, A. B.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1977
Subject Category
Aircraft Stability And Control
Report/Patent Number
NASA-CR-154122
Accession Number
77N28136
Funding Number(s)
CONTRACT_GRANT: NSG-1309
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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