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Aerodynamic Characteristics of an A-4B Aircraft with Simulated and Actual Gunfire Damage to One WingThe aerodynamic characteristics of a damaged McDonnell Douglas A-4B aircraft were studied in the Ames Research Center's 40- by 80-Foot Wind Tunnel. A standard fuselage and three different wings were used. The first wing tested was an undamaged one in which holes had been cut and detachable cover plates installed. Removal of one or more cover plates gave one of fourteen different simulated damage cases. The other two wings tested were damaged by actual gunfire at an Air Force range.
Document ID
19760023071
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Betzina, M. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Brown, D. H.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 3, 2013
Publication Date
July 1, 1976
Subject Category
Aerodynamics
Report/Patent Number
A-6519
NASA-TM-X-73119
Accession Number
76N30159
Funding Number(s)
PROJECT: RTOP 505-11-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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