A study of prediction methods for the high angle-of-attack aerodynamics of straight wings and fighter aircraft

Work is described dealing with two areas which are dominated by the nonlinear effects of vortex flows. The first area concerns the stall/spin characteristics of a general aviation wing with a modified leading edge. The second area concerns the high-angle-of-attack characteristics of high performance...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Mcmillan, O. J., Mendenhall, M. R., Perkins, S. C., Jr
Format:	Report
Sprache:	eng
Schlagworte:	Aerodynamics
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