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Technical

Report

Experimental data base for computer program assessment: Report of the Fluid Dynamics Panel Working Group 04

AGARD-AR-138

The acquisition of highly reliable wind tunnel test data for aircraft design was investigated.

Published1/5/1979
STOAuthorExternal
STOPublicationTypeTechnical Report RDP
Publication_ReferenceAGARD-AR-138
DOI
ISBNISBN-92-835-1323-1
STOPublisherAGARD
AccessOpen Access
STOKeywordsaircraft design; transonic flow; wind tunnel tests; aircraft configurations; data acquisition; three dimensional flow; two dimensional flow

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Experimental data base for computer program assessment: Report of the Fluid Dynamics Panel Working Group 041/5/1979Open Access