Supersonic Starting Flow by Accelerated Sinking Movement to Large Angle of Attack

The classic linear Heaslet–Lomax problem, which is concerned with the indicial response of a supersonic airfoil experiencing a sudden small step motion, was recently extended to nonlinear cases where the sudden step motion is of high amplitude or equivalently a high angle of attack is suddenly achie...

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Veröffentlicht in:	AIAA journal 2019-05, Vol.57 (5), p.1988-2000
Hauptverfasser:	Bai, Chen-Yuan, Li, Sheng, Wu, Zi-Niu
Format:	Artikel
Sprache:	eng
Schlagworte:	Acceleration Aerodynamics Angle of attack Computational fluid dynamics Computer simulation Elastic waves Evolution Flow Fluid dynamics High angle of attack Hydrodynamics Shock waves Superposition (mathematics) Supersonic airfoils
Online-Zugang:	Volltext
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