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Effects of simulated wing damage on the aerodynamic characteristics of a swept-wing airplane modelSimulated wing damage effects on aerodynamic characteristics of swept-wing airplane model
Document ID
19680012533
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hayes, C. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1968
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-1550
Report Number: NASA-TM-X-1550
Accession Number
68N22002
Funding Number(s)
CONTRACT_GRANT: 126-13-02-04-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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