Some aspects of streamwise vortex behavior during oblique shock wave/vortex interaction

Shock Waves

Volumn 8, Issue 4, 1998, Pages 243-255

  Smart, M K ^a   Kalkhoran, I M ^b   Popovic, S ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b POLYTECHNIC UNIVERSITY   (United States)

Author keywords

Shock wave; Shock wave interactions; Vortex; Vortical interactions

Indexed keywords

EID: 0342973573     PISSN: 09381287     EISSN: None     Source Type: Journal    
DOI: 10.1007/s001930050117     Document Type: Article

References (21)

1. Benjamin TB (1962) Theory of the Vortex Breakdown Phenomenon. Journal of Fluid Mechanics 14: 593-629
2. Cattafesta LN, Settles GS (1992) Experiments on Shock/Vortex Interaction. AIAA Paper 92-0315
3. Corpening G, Anderson J (1989) Numerical solutions to three-dimensional shock wave/vortex interaction at hypersonic speeds. AIAA paper 89-0674
4. Delery JM (1994) Aspects of vortex breakdown. Prog. Aerospace Sciences 30: 1-59
5. Delery JM, Horowitz E, Leuchter O, Solignac JL (1984) Fundamental studies on vortex flows. La Recherche Aerospatiale 2: 1-24
6. Hall MG (1972) Vortex breakdown. Annual Review of Fluid Mechanics 4: 195-218
7. Kalkhoran IM, Smart MK, Betti A (1996) Interaction of a supersonic wing-tip vortex with a normal shock. AIAA J. 34, 9: 1855-1861
8. Kalkhoran IM, Sforza PM (1994) Airfoil pressure measurements during oblique shock wave-vortex interaction in a Mach 3 stream. AIAA J. 32, 4: 783-788
9. Kalkhoran IM (1994) Vortex distortion during vortex-surface interaction in a Mach 3 stream. AIAA J. 32, 1: 123-129
10. Kandil OA, Kandil HA, Liu CH (1991) Supersonic quasiaxisymmetric vortex breakdown. AIAA Paper 91-3311
11. Leibovich S (1983) Vortex stability and breakdown: Survey and extension. AIAA J. 22, 9: 1192-1206
12. Metwally O, Settles G, Horstman C (1989) An experimental study of shock wave/vortex interaction. AIAA Paper 89-0082
13. Moeckel A (1952) Interaction of oblique shock waves with non-uniform regions. NACA TN 2725
14. Nedungadi A, lewis MJ (1996) Computational study of the flowfields associated with oblique shock/vortex interactions. AIAA J. 34, 11: 2545-2553
15. Rizzetta DP (1995) Numerical simulation of oblique shock-wave/vortex interaction. AIAA J. 33, 8: 1441-1446
16. Rizzetta DP (1997) Numerical simulation of vortex-induced shock-wave distortion. AIAA J. 35, 1: 209-211
17. Smart MK, Kalkhoran IM (1995a) The effect of shock strength on oblique shock wave-vortex interaction. AIAA J. 33, 11: 2137-2143
18. Smart MK, Kalkhoran IM (1995b) Calculation of shock wave propagation through non-uniform regions. Polytechnic University, Dept. of Aerospace Engineering, Brooklyn NY. POLY AE Report 95-04, August 1995
19. Smart MK, Kalkhoran IM, Bentson J (1995) Measurements of supersonic wing-tip vortices. AIAA J. 33, 10: 1761-1768
20. Squire HB (1960) Analysis of 'Vortex breakdown' phenomenon. Part I, Imperial College of Science and Technology, Aeronautics Department, Report No. 102, July 1960
21. Zatoloka V, Ivanyushkin AK, Nikolayev AV (1978) Interference of vortexes with shocks in airscoops. dissipation of vortexes. Fluid Mechanics, Soviet Research, 7, 4: 153-158