Navier-stokes predictions of hypersonic double-cone and cylinder-flare flow fields

39th Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2001, Pages

  Candler, Graham V ^a   Nompelis, Loannis ^a   Druguet, Marie Claude ^a,b  

^a UNIVERSITY OF MINNESOTA   (United States)

^b AIX MARSEILLE UNIVERSITÉ   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BENCHMARK DATASETS; NON-CONTINUUM EFFECTS; NUMERICAL FLUX EVALUATION; PARAMETRIC STUDY; RESEARCH CENTER; SEPARATED REGION; VIBRATIONAL EXCITATION; WORKING GROUPS;

AEROSPACE ENGINEERING; CONES; CYLINDERS (SHAPES); DATA PROCESSING; EXPERIMENTS; HYPERSONIC FLOW; LAMINAR FLOW; STATISTICAL TESTS;

COMPUTATIONAL FLUID DYNAMICS;

EID: 84897879272     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)

1. Wright, M.J, K. Sinha, and G.V. Candler, The Effect of Turbulence on Double-Cone Shock Interactions, AIAA Paper No. 99-0146, Jan. 1999.
2. Olejniczak, J., G.V. Candler, and H.G. Hornung, Computation of Double-Cone Experiments in High Enthalpy Nitrogen, AIAA Paper No. 97-2549, June 1997.
3. Olejniczak, J., G.V. Candler, M.J. Wright, I. Leyva, and H. Hornung, An Experimental and Computational Study of High Enthalpy Double-Wedge Flows, Journal of Thermophysics and Heat Transfer, Vol. 13, No. 4, pp. 431-440, Oct.-Dec. 1999.
4. Moss, J.N., and J. Olejniczak, Shock-Wave/Boundary Layer Interactions in Low Density Flows, AIAA Paper No. 98-2668, June 1998.
5. Chanetz, B., Study of Axisymmetric Shock Wave /Boundary Layer Interaction in Hypersonic Laminar Flows, ONERA Technical Report RT 42/4623AN, Feb. 1995.
6. Chanetz, B., R. Benay, J.-M. Bousquet, R. Bur, J. Oswald, T. Pot, F. Grasso, and J. Moss, Experimental and Numerical Study of the Laminar Separation in Hypersonic Flow, Aerospace Science and Technology, No. 3, pp. 205-218, 1998
7. Holden, M.S., Experimental Studies of Laminar Separated Flows Induced by Shock Wave/Boundary Layer and Shock/Shock Interaction in Hypersonic Flows for CFD Validation, AIAA Paper No. 2000-0930, Jan. 2000.
8. Holden, M.S., Experimental Measurements over Cone/Cone and Cylinder/Flare Configurations in Laminar Hypervelocity Flows, AIAA Paper No. 2000-1031, Jan. 2001.
9. MacCormack, R.W. and G.V. Candler, The Solution of the Navier-Stokes Equations Using Gauss-Seidel Line Relaxation, Computers and Fluids Vol. 17, No. 1, pp. 135-150, 1989
10. Candler, G.V. and R.W. MacCormack, The Computation of Hypersonic Ionized Flows in Chemical and Thermal Nonequilibrium, Journal of Thermo-physics and Heat Transfer, Vol. 5, No. 3, pp. 266-273, July 1991.
11. Wright, M.J., D. Bose, and G.V. Candler, A Data Parallel Line Relaxation Method for the Navier- Stokes Equations, AIAA Journal, Vol. 36, No. 9,PP- 1603-1609, Sept. 1998.
12. Sanders, R., E. Morano, M.-C. Druguet, Multidi- mensional Dissipation for Upwind Schemes: Stability and Applications Gas Dynamics, J. Comp. Phys., Vol. 145, No. 2, pp. 511-537, 1998
13. Holden, M.S., private communication
14. Candler, G.V., I. Nompelis, and M.S. Holden, Computational Analysis of Hypersonic Laminar Viscous-Inviscid Interactions, AIAA Paper No. 2000-0532, Jan. 2000
15. Boyd, I.D., G. Chen, and G.V. Candler, Predicting Failure of the Continuum Fluid Equations in Transitional Hypersonic Flows, Physics of Fluids, Vol. 7, No. 1, pp. 210-219, Jan. 1995.
16. Schaaf, S.A. and P.L. Chambre, Flow of Rarefied Gas Gases, Princeton Univ. Press, Princeton, NJ, 1966.