Time-accurate validation of the Chimera method for unsteady vortical flows

[1]  Miguel Visbal,et al.  Computational study of vortex breakdown on a pitching delta wing , 1993 .

[2]  S. Leibovich.  Vortex stability and breakdown - Survey and extension , 1984 .

[3]  R. F. Warming,et al.  An Implicit Factored Scheme for the Compressible Navier-Stokes Equations , 1977 .

[4]  Danesh K. Tafti,et al.  Vorticity dynamics and scalar transport in separated and reattached flow on a blunt plate , 1993 .

[5]  J. Steger,et al.  Implicit Finite-Difference Simulations of Three-Dimensional Compressible Flow , 1980 .

[6]  Pieter G. Buning,et al.  Development of a large scale Chimera grid system for the Space Shuttle Launch Vehicle , 1993 .

[7]  Robert L. Meakin,et al.  On the Spatial and Temporal Accuracy of Overset Grid Methods for Moving Body Problems , 1994 .

[8]  Man Mohan Rai,et al.  An implicit form for the Osher upwind scheme , 1986 .

[9]  M. Visbal.  Numerical investigation of laminar juncture flows , 1989 .

[10]  S. Leibovich.  THE STRUCTURE OF VORTEX BREAKDOWN , 1978 .

[11]  J. S. Shang,et al.  Thin-layer full Navier-Stokes simulations over a supersonic delta wing , 1991 .

[12]  Thomas H. Pulliam,et al.  Artificial Dissipation Models for the Euler Equations , 1985 .

[13]  L. Schiff,et al.  Vortical flows over delta wings and numerical prediction of vortex breakdown , 1990 .

[14]  Marcel Escudier,et al.  Vortex breakdown: Observations and explanations , 1988 .

[15]  Miguel R. Visbal,et al.  STRUCTURE OF LAMINAR JUNCTURE FLOWS , 1991 .