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Effects of variations in nose and windshield geometry on supersonic aerodynamic characteristics of a variable-sweep tactical fighter modelWindshield and nose geometry effects on supersonic aerodynamic characteristics of tactical fighter model
Document ID
19680027594
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Richardson, C. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
October 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-1664
Report Number: NASA-TM-X-1664
Accession Number
68N37066
Funding Number(s)
CONTRACT_GRANT: 720-01-00-18-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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