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Supersonic Leading Edge ReceptivityThis paper describes experimental studies of leading edge boundary layer receptivity for imposed stream disturbances. Studies were conducted in the supersonic T-325 facility at ITAM and include data for both sharp and blunt leading edges. The data are in agreement with existing theory and should provide guidance for the development of more complete theories and numerical computations of this phenomena.
Document ID
19980210014
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Maslov, Anatoly A.
(Institute of Theoretical and Applied Mechanics Novosibirsk Russia)
Date Acquired
September 6, 2013
Publication Date
June 1, 1998
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:208445
NASA/CR-1998-208445
Report Number: NAS 1.26:208445
Report Number: NASA/CR-1998-208445
Funding Number(s)
PROJECT: RTOP 282-10-01-01
CONTRACT_GRANT: NCC1-240
CONTRACT_GRANT: NCCw-74
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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