Panel method formulation for oscillating airfoils in supersonic flow

The mathematical model for two-dimensional unsteady supersonic flow based on the reduced potential equation, also known as the hyperbolic Helmholtz equation, is discussed.

Bibliographische Detailangaben

Veröffentlicht in:	AIAA journal 1995-09, Vol.33 (9), p.1659-1666
Hauptverfasser:	Soviero, Paulo A. O, Ribeiro, Renato S
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Applied fluid mechanics Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) Mathematical models Physics
Online-Zugang:	Volltext
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