Numerical study of inviscid shock interactions on double-wedge geometries

Journal of Fluid Mechanics

Volumn 352, Issue , 1997, Pages 1-25

  Olejniczak, Joseph ^a   Wright, Michael J ^a   Candler, Graham V ^a  

^a University of Minnesota   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLOW INTERACTIONS; GEOMETRY; JET AIRCRAFT; PRESSURE DROP; SHOCK WAVES;

DOUBLE WEDGE; INVISCID SHOCK INTERACTIONS; MACH NUMBER;

COMPUTATIONAL FLUID DYNAMICS;

EID: 0031362389     PISSN: 00221120     EISSN: None     Source Type: Journal    
DOI: 10.1017/S0022112097007131     Document Type: Article

References (8)

1. BERTIN, J. J. & HINKLE, J. C. 1975 Experimental investigation of supersonic flow past double wedge configurations AIAA J. 13, 897-901.
2. CANDLER, G. V., WRIGHT, M. J. & MCDONALD, J. D. 1994 Data-parallel lower-upper relaxation method for reacting flows. AIAA J. 32, 12, 2380-2386.
3. EDNEY, B. 1968 Anomalous heat transfer and pressure distributions on blunt bodies at hypersonic speeds in the presence of an impinging shock. Rep. 115. Flygtekniska Forsoksanstalten (The Aeronautical Research Institute of Sweden), Stockholm.
4. LAMONT, P. J. & HUNT, B. L. 1980 The impingement of underexpanded, axisymmetric jets on perpendicular and inclined plates J Fluid Mech 100, 471-511.
5. MACCORMACK, R. W. & CANDLER, G. V. 1989 The solution of the Navier-Stokes equations using Gauss-Seidel line relaxation. Computers Fluids 17, 135-150.
6. OLEJNICZAK, J. & CANDLER, G. V. 1996 Study of experiments sensitive to vibration-dissociation coupling models. Proc. 20th Intl Symp. on Shock Waves (ed. B. Sturtevant, J. E. Shepherd & H. G. Hornung), pp. 323-328. World Scientific.
7. OLEJNICZAK, J., CANDLER, G. V., WRIGHT, M. J., HORNUNG, H. G. & LEYVA, I. A. 1996 High enthalpy double-wedge experiments. AIAA Paper 96-2238.
8. OLEJNICZAK, J., WRIGHT, M. J. & CANDLER. G. V. 1996 Numerical study of shock interactions on double-wedge geometries. AIAA Paper 96-0041.