Solution of the unsteady Euler equations for fixed and rotor wing configurations

A solution procedure is described for the numerical solution of inviscid rotational flow past fixed and rotor wing configurations. This procedure solves the three-dimensional Euler equations in a body-fitted coordinate system and strong conservation form. The derivatives along the spanwise direction...

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Veröffentlicht in:	Journal of aircraft 1986-04, Vol.23 (4), p.283-289
Hauptverfasser:	Sankar, N. L, Wake, B. E, Lekoudis, S. G
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied fluid mechanics Euler equations Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) mechanics of gases Physics rotational flow wings
Online-Zugang:	Volltext
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