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Wind-tunnel-flight correlation of shock-induced separated flowDiscrepancies between wind tunnel predictions and actual flight test results for conditions of supercritical separated flow
Document ID
19660028007
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Loving, D. L. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
September 1, 1966
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-3580
Report Number: NASA-TN-D-3580
Accession Number
66N37297
Funding Number(s)
CONTRACT_GRANT: 126-13-03-22-23
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
FLIGHT TEST
SEPARATED FLOW
WIND TUNNEL

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