Computational analysis of viscous hypersonic flow over delta wings

Author:

Rizzi A.,Eliasson P.

Publisher

Springer Vienna

Reference11 articles.

1. Rizzi, A., Murman, E. M., Eliasson, P., Lee, M. K.: Calculation of hypersonic leeside vortices over blunt delta wings. In: Vortex Flow Aerodynamic., AGARD Conference Proceedings, CP-494, 1990.

2. Srinivasan, S., Eliasson, P., Rizzi, A.: Navier-Stokes computations of hypersonic flow past a blunt edge delta wing at several angles of attack. AIAA Paper 91–1698 (1991).

3. Srinivasan, S., Eliasson, P., Rizzi, A.: Hypersonic laminar flow computations over a blunt delta wing at three different chord Reynolds numbers. Proc. 9th GAMM Conf. Num. Meth. Fluid Mech. (Vos, J., Rizzi, A., Ryhming, I., eds.), pp. 152–160. Braunschweig: Vieweg 1992.

4. Squire, L. C.: Regimes over delta wings at supersonic and hypersonic speeds. Aero Q. 12, 1–14 (1976).

5. Miller, D. S., Wood, R. M.: Lee-side flow over delta wings at supersonic speeds. NASA TP 2430 (1985).

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