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Effects of boundary-layer treatment on cryogenic wind-tunnel controlsVarious techniques of realizing the desired boundary layer wall mass removal are considered in order to obtain the desired flow field over the model for various airfoils. The complementary problem of overall thermodynamic equilibrium maintenance created by the side wall boundary layer bleed is also addressed.
Document ID
19810003610
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Balakrishna, S.
(Old Dominion Univ. Norfolk, VA, United States)
Date Acquired
September 4, 2013
Publication Date
August 1, 1980
Subject Category
Research And Support Facilities (Air)
Report/Patent Number
NASA-CR-159372
Accession Number
81N12120
Funding Number(s)
CONTRACT_GRANT: NSG-1503
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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