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Effects of Additional Revisions on the Aerodynamic Characteristics of a Target Drone Vehicle at Mach Numbers from 1.70 to 4.63. COORD No. AF-AM-827Wind tunnel tests to determine supersonic aerodynamic characteristics of target drone aircraft
Document ID
19700016518
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Blair, A. B., Jr. (NASA Langley Research Center Hampton, VA, United States)
Tudor, D. H. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-SX-1961
Accession Number
70N25828
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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