Method is based on observation of divergence that occurs in variation of mean static pressure at trailing edge of aircraft wing at critical stage in development of boundary-layer separation when its influence first spreads to trailing edge and thereby to overall flow; various flow changes considered are illustrated by schlieren photographs. (Received 1960)
Method for prediction of onset of buffeting and other separation effects from wind tunnel tests on rigid models
AGARD -- Report
1958
93 pages
Report
Englisch
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Correlation of F-A-18 Buffeting from Wind-Tunnel and Flight Tests
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