An analysis of the lift augmentation due to a thin jet of air issuing from a slot along the leading edge of a delta wing is presented. The problem is treated with an extension of the method of Brown and Michael, representing the separated flow on the lee side of the wing by a pair of concentrated vortices and corresponding feeding sheets. It is assumed that the jet is not affected by Coanda forces. The analysis produces qualitative agreement with experiments.
The lift of sharp-leading-edged delta wings with blowing
01.12.1985
Report
Keine Angabe
Englisch
Lift of delta wings with leading-edge blowing
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