Unstructured multigrid simulations of axisymmetric inviscid launch vehicle flows

19th AIAA Applied Aerodynamics Conference

Volumn , Issue , 2001, Pages

  Strauss, Daniel ^a   Azevedo, João Luiz F ^b  

^a INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

^b INSTITUTO DE AERONÁUTICA E ESPAÇO   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW FIELDS; HYPERSONIC AERODYNAMICS; SUPERSONIC AIRCRAFT; TRANSONIC FLOW;

AGGLOMERATION MULTIGRID; CONVERGENCE ACCELERATION; LIOU FLUX-VECTOR SPLITTING SCHEMES; QUADRILATERAL MESHES; SECOND-ORDER ACCURACY; SPATIAL DISCRETIZATION SCHEMES; STEADY STATE SOLUTION; TANGENTIAL DIRECTIONS;

MESH GENERATION;

EID: 85067321731     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-2476     Document Type: Conference Paper

References (14)

1. Azevedo, J.L.F., Menezes, J.C.L., and Fico, N.G.C.R., Jr., An Assessment of Boundary Layer Properties for Transonic and Supersonic Flows Over the VLS, AIAA Paper 95-1769-CP, Proceedings of the 13th AIAA Applied Aerodynamics Conference, Part 1, San Diego, CA, June 1995, pp. 41-51.
2. Azevedo, J.L.F., Menezes, J.C.L., and Fico, N.G.C.R., Jr., Accurate Turbulent Calculations of Transonic Launch Vehicle Flows, AIAA Paper No. 96-2484-CP, Proceedings of the 14th AIAA Applied Aerodynamics Conference, Part 2, New Orleans, LA, June 1996, pp. 841-851.
3. Azevedo, J.L.F., Strauss, D., and Ferrari, M.A.S., Viscous Multiblock Simulations of Axisymmetric Launch Vehicle Flows, Journal of Spacecraft and Rockets, Vol. 36, No. 4, July-Aug. 1999, pp. 489-498.
4. Strauss, D., and Azevedo, J.L.F., A Numerical Study of Turbulent Afterbody Flows Including a Propulsive Jet, AIAA Paper No. 99-3190, Proceedings of the 17 th AIAA Applied Aerodynamics Conference, Norfolk, VA, June-July 1999, pp. 654-664.
5. +, NASA TM-106524, NASA Lewis Research Center, Cleveland, OH, Mar. 1994.
6. +, Journal of Computational Physics, Vol. 129, 1996, pp. 364-382.
7. Azevedo, J.L.F., and Korzenowski, H., Comparison of Unstructured Grid Finite Volume Methods for Cold Gas Hypersonic Flow Simulations, AIAA Paper No. 98-2629, Proceedings of the 16th AIAA Applied Aerodynamics Conference, Albuquerque, NM, June 1998, pp. 447-463.
8. Mavriplis, D.J., and Venkatakrishnan, V., Agglomeration Multigrid for Viscous Turbulent Flows, AIAA Paper No. 94-2332, 25th AIAA Fluid Dynamics Conference, Colorado Springs, June 1994.
9. Mavriplis, D.J., Multigrid Solution of the Two-Dimensional Euler Equations on Unstructured Triangular Meshes, AIAA Journal, Vol. 26, No. 7, 1988, pp. 824-831.
10. Mavriplis, D.J., Accurate Multigrid Solution of the Euler Equations on Unstructured and Adaptive Meshes, AIAA Journal, Vol. 28, No. 2, 1990, pp. 213-221.
11. Jameson, A., and Mavriplis, D.J., Finite Volume Solution of the Two-Dimensional Euler Equations on a Regular Triangular Mesh, AIAA Journal, Vol. 24, No. 4, April 1986, pp. 611-618.
12. Barth, T.J., and Jespersen, D.C., The Design and Application of Upwind Schemes on Unstructured Meshes, AIAA Paper No. 89-0366, 27th AIAA Aerospace Sciences Meeting, Reno, NV, 1989.
13. van Leer, B., Towards the Ultimate Conservative Difference Scheme. V. A Second-Order Sequel to Godunov's Method, Journal of Computational Physics, Vol. 32, No. 1, 1979, pp. 101-136.
14. Venkatakrishnan, V., Convergence to Steady State Solutions of the Euler Equations on Unstructured Grids with Limiters, Journal of Computational Physics, Vol. 118, 1995, pp. 120-130.