Numerical simulation of delta-wing roll

This paper presents computations of the flowfield around an 80° sweep delta wing undergoing a constant roll-rate manoeuver from 0° to 45°. The governing equations for the problem are the unsteady, three-dimensional Navier-Stokes equations. The equations are solved using the implicit, approximately-f...

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Veröffentlicht in:	Aerospace science and technology 1998-09, Vol.2 (6), p.347-357
Hauptverfasser:	Gordnier, Raymond E., Visbal, Miguel R.
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Applied fluid mechanics delta wing flow field dynamical behaviour Exact sciences and technology Fluid dynamics Fundamental areas of phenomenology (including applications) governing equation algorithm Navier-Stokes equation numerical simulation Physics vortex attack angle
Online-Zugang:	Volltext
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