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Effect of speed brakes on the supersonic aerodynamic characteristics of a variable sweep tactical fighter model at Mach numbers from 1.60 to 2.50Wind tunnel evaluation of speed brake effects on supersonic characteristics of variable sweep fighter aircraft models
Document ID
19680024197
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Richardson, C. S. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1968
Subject Category
Aircraft
Report/Patent Number
NASA-TN-D-4773
Accession Number
68N33669
Funding Number(s)
CONTRACT_GRANT: 126-13-02-20-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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