Viscous multiblock simulations of axisymmetric launch vehicle flows

Journal of Spacecraft and Rockets

Volumn 36, Issue 4, 1999, Pages 489-498

  Azevedo, João L F ^a   Strauss, Daniel ^b   Ferrari, Marcello A S ^a  

^a Inst de Aero e Espaco   (Brazil)

^b INSTITUTO TECNOLÓGICO DE AERONÁUTICA   (Brazil)

Author keywords

[No Author keywords available]

Indexed keywords

ALGORITHMS; APPROXIMATION THEORY; COMPUTER SIMULATION; MATHEMATICAL MODELS; NAVIER STOKES EQUATIONS; NUMERICAL ANALYSIS; TURBULENT FLOW; VISCOUS FLOW;

BALDWIN-BARTH MODEL; BALDWIN-LOMAX MODEL; BEAM-WARMING IMPLICIT APPROXIMATION FACTORIZATION ALGORITHM; LAUNCH VEHICLES;

ROCKET ENGINES;

EID: 0032650547     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/3.27190     Document Type: Article

References (21)

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," Proceedings of the AIAA 13th Applied Aerodynamics Conference, Pt. 1, AIAA, Washington, DC, 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," Proceedings of the AIAA 14th Applied Aerodynamics Conference, Pt. 2, AIAA, Reston, VA, 1996, pp. 841-851.
3. Nietubicz, C. J., Pulliam, T. H., and Steger, J. L., "Numerical Solution of the Azimuthal-Invariant Thin-Layer Navier-Stokes Equations," AIAA Paper 79-0010, Jan. 1979.
4. Deiwert, G. S., "Supersonic Axisymmetric Flow over Boattails Containing a Centered Propulsive Jet," AIAA Journal, Vol. 22, No. 10, 1984, pp. 1358-1365.
5. Zdravistch, F., and Azevedo, J L. F., "Numerical Simulation of High Speed Flows over Complex Satellite Launchers," Proceedings of the 3rd Brazilian Thermal Sciences Meeting, Vol. 1, Associação Brasileira de Ciências Mecânicas, Itapema, SC, Brazil, 1990, pp. 233-238.
6. Baldwin, B. S., and Lomax, H., "Thin Layer Approximation and Algebraic Model for Separated Turbulent Flows," AIAA Paper 78-257, Jan. 1978.
7. Johnson, D. A., and King, L. S., "A Mathematically Simple Turbulence Closure Model for Attached and Separated Turbulent Boundary Layers," AIAA Journal, Vol. 23, No. 11, 1985, pp. 1684-1692.
8. Baldwin, B. S., and Barth, T. J., "A One-Equation Turbulence Transport Model for High Reynolds Number Wall-Bounded Flows," NASA TM-102847, Aug. 1990.
9. Beam, R. M., and Warming, R. F., "An Implicit Factored Scheme for the Compressible Navier-Stokes Equations," AIAA Journal, Vol. 16, No. 4, 1978, pp. 393-402.
10. Pulliam, T. H., and Steger, J. L., "Implicit Finite Difference Simulations of Three-Dimensional Compressible Flow," AIAA Journal, Vol. 18, No. 2, 1980, pp. 159-167.
11. Pulliam, T. H., "Artificial Dissipation Models for the Euler Equations," AIAA Journal, Vol. 24, No. 12, 1986, pp. 1931-1940.
12. Azevedo, J. L. F., Moraes, P., Jr., Maliska, C. R., Marchi, C. H., and Silva, A. F. C., "Code Validation for High-Speed Flow Simulation over Satellite Launch Vehicle," Journal of Spacecraft and Rockets, Vol. 33, No. 1, 1996, pp. 15-21.
13. Fernandez, F. Z., "Simulação de Escoamentos Aerodinâmicos em Configurações Tipo Cluster" ("Simulation of Aerodynamic Flows over Cluster Type Configurations"), M.S. Dissertation, Dept. of Aeronautical Engineering, Inst. Tecnológico de Aeronáutica, São José dos Campos, SP, Brazil, Nov. 1990.
14. Menezes, J. C. L., "Análise Numérica de Escoamentos Transônicos Turbulentos em Torno de Aerofólios" ("Numerical Analysis of Transonic Turbulent Flows About Airfoils"), M.S. Dissertation, Dept. of Aeronautical Engineering, Inst. Tecnológico de Aeronáutica, São José dos Campos, SP, Brazil, July 1994.
15. Shirazi, S. A., and Truman, C. R., "A Study of Algebraic and Half-Equation Turbulence Models for Hypersonic PNS Predictions," AIAA Paper 88-0222, Jan. 1988.
16. Azevedo, J. L. F., Fico, N. G. C. R., Jr., Ortega, M. A., and Luna, G. C., "Nozzle Flow Computations Using the Euler Equations," Proceedings of the 18th Congress of the International Council of the Aeronautical Sciences, Vol. 1, International Council of the Aeronautical Sciences, Washington, DC, 1992, pp. 97-107.
17. Azevedo, J. L. F., Fico, N. G. C. R., Jr., and Ortega, M. A., "Two-Dimensional and Axisymmetric Nozzle Flow Computations Using the Euler Equations," Journal of the Brazilian Society of Mechanical Sciences, Vol. 17, No. 2, 1995, pp. 147-170.
18. Gregório, E. L., "Simulação Numérica de Escoamentos em Regiões Traseiras de Veículos Lançadores" ("Numerical Simulation of Flows in the Afterbody Region of Launch Vehicles"), Graduation Project, Dept. of Aeronautical Engineering, Inst. Tecnológico de Aeronáutica, São José dos Campos, SP, Brazil, Nov. 1995.
19. Fletcher, C. A. J., Computational Techniques for Fluid Dynamics 2. Specific Techniques for Different Flow Categories, Springer-Verlag, Berlin, 1988, pp. 101-109.
20. Merz, R. A., Page, R. H., and Przirembel, C. E. G., "Subsonic Axisymmetric Near-Wake Studies," AIAA Journal, Vol. 16, No. 7, 1978, pp. 656-662.
21. Herrin, J. L., and Dutton, J. C., "Supersonic Base Flow Experiments in the Wake of a Cylindrical Afterbody," AIAA Journal, Vol. 32, No. 1, 1994, pp. 77-83.