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Inverse transonic airfoil design methods including boundary layer and viscous interaction effectsThis report covers the period 1 September 1983 to 31 January 1984. The primary task during this reporting period was the continued development of the massive separation model and computer code (SKANSEP). In particular, detailed investigations were conducted with the boundary layer displacement surface correction technique discovered near the end of the last reporting period. This report will present detailed results using this technique and show comparisons with experimental data.
Document ID
19840013446
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Carlson, L. A.
(Texas A&M Univ. College Station, TX, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1984
Subject Category
Aerodynamics
Report/Patent Number
NAS 1.26:173449
NASA-CR-173449
TAMRF-3224-84-01
Accession Number
84N21514
Funding Number(s)
CONTRACT_GRANT: NSG-1174
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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