J.M.A. Longo, A. Das

A numerical study of the vortical flow field of a double-delta wing moving in a viscous compressible medium is performed. The method followed is a finite volume cell-vertex scheme and the solution procedure was based on thin layer approximations. The turbulent shear stresses are derived by using Baldwin-Lomax modell. Extensive experimental data have been available to validate all the numerical results, showing quite good agreements.

7. DGLR-Fach-Symposium, 1990, Aachen

Conference Paper

englisch

14,8 x 21,0 cm, 4 Seiten

DGLR-Bericht, 1990, 1990-06, Strömung mit Ablösung; S.186-189; 1990; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

aerodynamics

Bestellbar

1990