Abstract
The near term availability of scientific supercomputers will soon permit routine simulation of three dimensional compressible flow about relatively complex configurations.
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References
Beam, R. M. and Warming, R. F., An Implicit Finite - Difference Algorithm for Hyperbolic Systems in Conservation - Law - Form, J. Comp. Phys. 22 (Sept. 1976,), p. 87–110.
Warming, R. F. and Beam, R. M., On the Construction and Application of Implicit Factored Schemes for Conservation Laws, Symposium of CFD, New York, 11 (April 16–17, 1977, SIAM-AMS Proceedings).
Steger, J. L., Implicit Finite Difference Simulation of Flow About Arbitrary Two Dimensional Geometries, AIAA J. 16, No. 7 (July 1978).
Pulliam, T. H. and Steger, J. L., On Implicit Finite Difference Simulations of Three Dimensional Flows, AIAA J. 18 (Feb. 1980).
Pulliam, T. H., Euler and Thin Layer Navier Stokes Codes: ARCED, ARCED, Notes for Computational Fluid Dynamics User’s Workshop, The University of Tennessee Space Institute, Tullahoma, Tenn. (March 12–16, 1984).
Pulliam, T. H. and Steger, J. L., Recent Inprovements in Efficiency, Accuracy, and Convergence of an. Implicit Approximate Factorization Algorithm, AIAA Paper 85–0360 (Jan. 1985).
Viviand, H., Conservative Forms of Gas Dynamics Equations, La Recherche Aerospatiale 1 (1978).
Thomas, P. D. and Lombard, C. K., Geometric Conservation Law and Its Application to Flow Computations on Moving Grids, AIAA Journal 17 (1979).
Steger, J. L., Pulliam, T. H. and Chima, R. V., An Implicit Finite Difference Code for Inviscid and Viscous Cascade Flow, AIAA paper 80–1427 (1980).
Pulliam, T. H., Characteristic Boundary Conditions for the Euler Equations, NASA Publication 2201, Numerical Boundary Condition Procedures (Oct. 1980).
Chakravarthy, Euler Equations - Implicit Schemes and Implicit Boundary Conditions, AIAA 82–0228 (Jan. 11–14, 1982).
Schiff, L. B. and Steger, J. L., Numerical Simulation of Steady Supersonic Viscous Flow, AIAA Journal 18 (Dec. 1980).
Nicolet, W. E., Shanks, S., Srinivasan, G. and Steger, J. L., Flowfield Predictions About Lifting Entry Vehicles, AIAA Paper 82–0026 (Jan. 11–14, 1982).
Lomax, H. and Pulliam, T. H., A Fully Implicit Factored Code for Computing Three - Dimensional Flows on the ILLIAC IV, Parallel Computations, G. Rodrigue, Ed. Academic Press, New York (1982).
Pulliam, T. H. and Chaussee, D. S., A Diagonal Form of an Implicit Approximate - Factorization Algorithm, J. Comp. Phys. 39, no. 2 (Feb. 1981), p. 347.
Chaussee, D. S. and Pulliam, T. H., A Diagonal Form of an Implicit Approximate Factorization Algorithm with Application to a Two Dimensional Inlet, AIAA J. 19, no. 2 (Feb. 1981), p. 153.
Barth, T. J. and Steger, J. L., An Efficient Approximate Factorization Implicit Scheme for the Equations of Gasdynamics, NASA TM 85957 (June 1984).
Eberhardt, D. S., A Study of Multiple Grid Problems on Concurrent Processing Computers, Stanford University Dissertation, Department of Aeronautics and Astronautics, Stanford, CA. (Sept., 1984).
Reddy, K. C., Pseudospectral Approximation in a Three - Dimensional Navier - Stokes Code, AIAA J. 21, no. 8 (Aug. 1983).
Yee, H. C., Warming, R. F. and Harten, A., Implicit Total Variation Diminishing (TVD) Schemes for Steady - State Calculations, NASA TM 84342 (March 1983).
Chow, L. J., Pulliam, T. H. and Steger J. L., A General Perturbation Approach for the Equations of Fluid Dynamics, AIAA Paper 83–1903 (July 13–15, 1983).
Anderson, W. K., Thomas, J. L. and Rumsey, C. L., Application of Thin Layer Navier - Stokes Equations Near Maximum Lift, AIAA Paper 84–0049 (Jan. 1984).
Barth, T. J., Pulliam, T. H. and Buning, P., Navier - Stokes Computations for Exotic Airfoils, AIAA Paper 85–0109 (Jan. 1985).
Barton, J. T. and Pulliam, T. H., Airfoil Computations at High Angles of Attack, Inviscid and Viscous Phenomena, AIAA Paper 84–0524 (1984).
Srinivasan, G. R., McCroskey, W. J. and Kutler P., Numerical Simulation of the Interaction of a Vortex with Stationary Airfoil in Transonic Flow, AIAA Paper 84–0254 (Jan. 1984).
Nietubicz, C. J., Navier Stokes Computations for Conventional and Hollow Projectile Shapes at Transonic Velocities, AIAA Paper 81–1262 (June 1981).
Sahu, J., Nietubicz, C. J. and Steger, J. L., Numerical Computation of Base Flow for a Projectile at Transonic Speeds, AIAA 82–1358 (Aug. 9–11, 1982).
Kutler, P., Pedelty, J. A. and Pulliam, T. H., Supersonic Flow over Three - Dimensional Ablated Nosetips Using an Unsteady Implicit Numerical Procedure, AIAA Paper 80–0063 (1980).
Mansour, N. N., Numerical Simulation of the Tip Vortex Off a Low - Aspect Ratio Wing at Transonic Speed, AIAA Paper 84–0522 (Jan. 1984).
Diewert, G. S., Topological Analysis of Computed Three -Dimensional Viscous Flow Fields, In `Recent Contributions to Fluid Mechanics’, W. Haase, ed. Springer-Verlag, Berlin (1982).
Chaussee, D. S., Rizk, Y. M. and Buning, P. G., Viscous Computation of a Space Shuttle Flow Field, NASA TM 85977 (June 1984).
Baldwin, B. S. and Lomax, H., Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows, AIAA Paper 78–257 (Jan. 1978).
Steger, J. L. and Warming, R. F., Flux Vector Splitting of the Inviscid Gasdynamics Equations with Applications to Finite Difference Methods, J. of Comp. Physics 40 (1981).
Buning, P. G., Computation of Inviscid Transonic Flow Using Flux Vector Splitting in Generalized Coordinates, Stanford University Dissertation, Department of Aeronautics and Astronautics, Stanford, CA (1983).
Anderson, W. K., Thomas, J. L. and Van Leer, B., A Comparison of Finite Volume Flux Vector Splittings for the Euler Equations, AIAA Paper 85–0122 (Jan. 1985).
Chakravarthy, S. R. and Osher, S., Numerical Experiments with the Osher Upwind Scheme for the Euler Equations, AIAA Paper 82–0975 (June 1982).
Chakravarthy, S. R. and Osher, S., High Resolution Applications of the Osher Upwind Scheme for the Euler Equations, AIAA Paper 83–1943 (1983).
Clarke, D. K., Hassan, H. A. and Salas, M. D., Euler Calculations for Multielement Airfoils Using Cartesian Grids, AL4A Paper 85–0291 (Jan. 1985).
Lasinski, T. A., et. al., Computation of the Steady Viscous Flow Over a Tri-Element Augmenter Wing Airfoil„ AIAA Paper 82–0021 (Jan. 1982).
Rai, M. M., A Conservative Treatment of Zonal Boundaries for Euler Equation Calculations, AIAA Paper 84–0164 (1984).
Hessenius, K. A. and Rai, M. M., Applications of a Conservative Zonal Scheme to Tansient and Geometrically Complex Problems, AIAA Paper 84–1532 (June 1984).
Atta, E. H. and Vadyak, T., A Grid Interfacing Zonal Algorithm for Three Dimensional Transonic Flows About Aircraft Configurations, AIAA Paper 82–1017 (June 1982).
Steger, J. L., Dougherty, F. C. and Benek, J. A., A Chimera Grid Scheme, ASME Mini-Symposium on Advances in Grid Generation, Houston, Texas, (June 1983).
Benek, J. A., Steger, J. L. and Dougherty, F. C., A Flexible Grid Embedding Technique with Application to the Euler Equations, AIAA 83–1944 (July 13–15, 1983).
Berger, M. J., Adaptive Mesh Refinement for Hyperbolic Partial Differential Equations, STAN-CS-82–924, Stanford University (Aug. 1982).
Dougherty, F. C., Development of a Chimera Grid Scheme with Applications to Unsteady Problems, Stanford University Dissertation, Department of Aeronautics and Astronautics, Stanford, CA (Oct. 1984).
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Steger, J.L., Buning, P.G. (1985). Developments in the Simulation of Compressible Inviscid and Viscous Flow on Supercomputers. In: Murman, E.M., Abarbanel, S.S. (eds) Progress and Supercomputing in Computational Fluid Dynamics. Progress in Scientific Computing, vol 6. Birkhäuser Boston. https://doi.org/10.1007/978-1-4612-5162-0_5
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DOI: https://doi.org/10.1007/978-1-4612-5162-0_5
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