Use of this analytical parameter, it is shown, highlights the distinction between cases which are dominated by trailing-edge separation, and those for which separation at the shock foot is dominant. Use of the analytical parameter and the distinction noted above greatly improves the correlation of separation data and the extrapolation of wind tunnel data to flight conditions.
New considerations on scale extrapolation of wing pressure distributions affected by transonic shock-induced separations
1983-03-01
Report
No indication
English
Reynolds Number Extrapolation of Transonic Wing Pressure Data Affected by Shock-Induced Separation
SAE Technical Papers | 1986
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