Shock unsteadiness model applied to hypersonic shock-wave/turbulent boundary layer interactions

Collection of Technical Papers - 44th AIAA Aerospace Sciences Meeting

Volumn 3, Issue , 2006, Pages 1622-1633

  Sinha, Krishnendu ^a,b  

^a INDIAN INSTITUTE OF TECHNOLOGY MADRAS   (India)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

MACH NUMBER; NAVIER STOKES EQUATIONS; REYNOLDS NUMBER; SHOCK WAVES; TURBULENT FLOW; UNSTEADY FLOW;

CONE-FLARE JUNCTION; TURBULENT BOUNDARY LAYER; UNSTEADINESS MODEL;

BOUNDARY LAYER FLOW;

EID: 34250730658     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2006-126     Document Type: Conference Paper

References (12)

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3. Coakley, T.J., and Huang, P.G., "Turbulence Modeling for High Speed Flows," AIAA Paper 92-0436, Jan. 1992.
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8. Wilcox, D.C., Turbulence modeling for CFD, DCW Industries, Inc., La Canada, CA, 1998, pp. 236-239.
9. Spalart, P.R., and Allmaras, S.R., "A One-Equation Turbulence Model for Aerodynamic Flows," AIAA Paper 92-0439, Jan. 1992.
10. MacCormack, R. W. and Candler, G. V., "The Solution of the Navier-Stokes Equations Using Gauss-Seidel Line Relaxation," Computers and Fluids, Vol. 17, No. 1, 1989, pp. 135-150.
11. Sinha, K. and Candler, G.V., "An Accurate Implicit Formulation of a Two-Equation Turbulence Model," AIAA Paper 98-2649, June 1998.
12. Wright, M. J., Candler, G. V., and Bose, D., "Data-Parallel Line Relaxation Method for the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, 1998, pp. 1603-1609.