Numerical simulation of the integrated space shuttle vehicle in ascent

15th Atmospheric Flight Mechanics Conference, 1988

Volumn , Issue , 1988, Pages 265-283

  Buning, P G ^a   Chiu, I T ^a,b   Obayashi, S ^a   Rizk, Y M ^a,c   Steger, J L ^a  

^a NASA AMES RESEARCH CENTER   (United States)

^b IOWA STATE UNIVERSITY   (United States)

^c Iowa State Univ ^*  (India)

Author keywords

[No Author keywords available]

Indexed keywords

FLIGHT SIMULATORS; SPACE SHUTTLES; WIND TUNNELS;

COMPUTATIONAL RESULTS; FLIGHT CONDITIONS; FLIGHT TEST DATA; GEOMETRIC COMPONENT; GRID DISCRETIZATION; NUMERICAL ERRORS; THIN LAYER NAVIER STOKES EQUATIONS;

NAVIER STOKES EQUATIONS;

EID: 84997815805     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.1988-4359     Document Type: Conference Paper

References (23)

1. Steger, J. L., Dougherty, F. C. and Benek, J. A.: A Chimera Grid Scheme, in Advances in Grid Generation, K.N. Ghia and U. Chia, Eds., ASME FED-5, 59-69, 1983.
2. Benek, J. A., Buning, P. G., and Steger, J. L.: A 3-D Grid Embedding Technique. AIAA Paper No. 85-1523, July 1985.
3. Dougherty, F. C, Benek, J. A., and Steger, J. L.: On Application of Chimera Grid Scheme to Store Separation, NASA TM 88193, Oct. 1985.
4. Benek, J. A., Donegan, T. L., and Suhs, N. E.: Extended Chimera Grid Embedding Scheme with Application to Viscous Flows. AIAA-87-1126-CP, June, 1987.
5. Ying, S. X., Steger, J. L., Schiff, L. B., and Baganoff, D.: Numerical Simulation of Unsteady, Viscous, High Angle of Attack Flows Using a Partially Flux-Split Algorithm. AIAA Paper No. 86-2179, Aug. 1986.
6. Steger, J. L., Ying, S. X., and Schiff, L.B.: A Partially Flux-Split Algorithm for Numerical Simulation of Compressible Inviscid and Viscous Flow. Proceedings of the Workshop on Computational Fluid Dynamics, Institute of Nonlinear Sciences, University of California, Davis, California, 1986.
7. Benek, J. A., Steger, J. L., Dougherty, F. C. and Buning P. G., Chimera: A Grid Embedding Technique, AEDC-TR-85-64, Arnold Air Force Station, TN, 1986.
8. Steger, J. L. and Benek, J. A., On the Use of Composite Grid Schemes in Computational Aerodynamics, Computer Methods in Applied Mechanics and Engineering, Vol. 64, Nos. 1-3, Oct. 1987, pp. 301-320
9. Steger, J. L. and Chaussee, D. S., Generation of Body Fitted Coordinates Using Hyperbolic Partial Differential Equations, SIAM Journal Sci. Stat. Comput., Vol. 1, No. 4, Dec. 1980, pp. 431-437.
10. Kinsey, D. W. and Barth, T. J., Description of a Hyperbolic Grid Generation Procedure for Arbitrary Two-Dimensional Bodies, AFWAL Technical Memorandum, No.84-191-FIMM, July, 1984
11. Steger, J. L and Rizk, Y. M.: Generation of Three Dimensional Body Fitted Coordinates Using Hyperbolic Partial Differential Equations. NASA TM 86753, June, 1985.
12. Rizk, Y. M. and Ben-shmuel, S.: Computation of the Viscous Flow Around the Shuttle Orbiter at Low Supersonic Speeds. AIAA Paper 85-0168, Jan. 1985.
13. Rizk, Y. M., Steger, J. L. and Chaussee, D., Use of a Hyperbolic Grid Generation Scheme in Simulating Supersonic Viscous Flow About Three-Dimensional Winged Configurations, NASA TM 86776, July, 1985.
14. Pulliam, T. H. and Steger, J. L., On Implicit Finite-Difference Simulations of Three Dimensional Flow, AIAA Paper No. 78-10, Huntsville, Ala., Jan., 1978.
15. Baldwin, B. S. and Lomax, H.: Thin Layer Approximation and Algebraic Model for Separated Turbulent Flow, AIAA Paper No. 78-257, Jan. 1978.
16. Thomas, J. L., Taylor, S. L. and Anderson, W. K. Navier-Stokes Computations of Vortical Flows over Low Aspect Ratio Wings, AIAA Paper No. 87-0207, AIAA 25th Aerospace Sciences Meeting, Jan. 12-15, 1987.
17. Vinokur, M., An Analysis of Finite-Difference and Finite-Volume Formulations of Conservation Laws, NASA Contractor Report 177416, June, 1986.
18. Chakravarthy, S. R. and Sezma, K. Y., An Euler Solver for Three-Dimensional Supersonic Flows with Subsonic Pockets, AIAA Paper No. 85-1703, July, 1985.
19. Kaynak, U., Hoist, T. L., and Cant well, B. J., Computation of Transonic Separated Wing Flows Using an Euler/Navier-Stokes Zonal Approach, NASA TM 88311, July, 1986.
20. Spangler, R. H.: Results of Tests Using a 0.03 Scale Model (47-OTS) of the Space Shuttle Integrated Vehicle in the AEDC 16 Foot Transonic Propulsion Wind Tunnel (IA105A), Vol. 2 of 3, NASA Contractor Report 160851, Oct. 1981.
21. Rockwell International Internal Letter SAS / AERO 83-094, “STS-5 Postflight Report on Ascent External Aerodynamic Loads”, March 1983.
22. Obayashi, S.: Numerical Simulation of Underex-panded Plumes using Upwind Algorithms, AIAA Paper 88-4360, 1988.
23. Szema, K. Y., Chakravarthy, S. R., Riba, W. T., Byerly, J. and Dresser, H. S., Multi-Zone Euler Marching Technique for Flow Over Singe and Multi-Body Configurations, AIAA Paper No. 87-0592, AIAA 25th Aerospace Sciences Meeting, Jan. 12-15, 1987.