Navier-Stokes calculations of transonic flows past cavities

S Srinivasan, O Baysal - 1991 - asmedigitalcollection.asme.org
Presented in this paper is a computational investigation of subsonic and transonic flows past
three-dimensional deep and transitional cavities. Simulations of these self-induced …

Calculation of external-internal flow fields for mixed-compression inlets

WJ Chyu, T Kawamura, DP Bencze - Computer Methods in Applied …, 1987 - Elsevier
Supersonic inlet flows with mixed external-internal compressions were computed using a
combined implicit-explicit (Beam-Warming-Steger/MacCormack) method for solving the …

Numerical solution of the Navier-Stokes equations about three-dimensional configurations: A survey

TL Holst - Supercomputing in Aerospace, 1987 - ntrs.nasa.gov
The numerical solution of the Navier-Stokes equations about three-dimensional
configurations is reviewed. Formulational and computational requirements for the various …

[图书][B] Convergence acceleration of upwind relaxation methods for the Navier-Stokes equations

AC Taylor III - 1989 - search.proquest.com
Two methods for improving the computational efficiency of upwind relaxation algorithms for
the Navier-Stokes equations are proposed and tested. The purpose of the work is the …

Structured and unstructured grid adaptation schemes for numerical modeling of field problems

R Ramakrishnan - Applied Numerical Mathematics, 1994 - Elsevier
The use of grid adaptation procedures for compressible flows and heat transfer is presented
in this paper. Grid adaptation schemes are presented for structured and unstructured grids in …

Navier-Stokes calculations of transonic flows past cavities

O Baysal, S Srinivasan - 1989 - ntrs.nasa.gov
A computational investigation of subsonic and transonic flows past 3-D deep transitional
cavities is presented. Computational simulations of these self-induced oscillatory flows were …

CFD for hypersonic airbreathing aircraft

A Kumar - 11th International Conference on Numerical Methods …, 2005 - Springer
A general discussion is given on the use of advanced computational fluid dynamics (CFD) in
analyzing the hypersonic flow field around an airbreathing aircraft. Unique features of the …

Analytical and experimental evaluation of a 3-D hypersonic fixed-geometry, swept, mixed compression inlet

A AGNONE - 25th AIAA Aerospace Sciences Meeting, 1987 - arc.aiaa.org
The performance of a fixed-geometry, swept, mixed compression hypersonic inlet is
presented. The experimental evaluation was conducted for a Mach number of 6.0 and for …

[引用][C] Numerical simulations of flow field around three-dimensional complex configurations

S Ogawa, T Ishiguro, Y Takakura - GAMM-Conference on Numerical Methods in Fluid …, 1987