Tip clearance vortex development and shock-vortex-interaction in a transonic axial compressor rotor

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Hofmann, W ^a   Ballmann, J ^a  

^a RWTH AACHEN UNIVERSITY   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0141646147     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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8. FINE™Numeca's Flow Integrated Environment, User Manual FINE™, April 2000.
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10. Rizzetta, D.P., Numerical Simulation of Vortex-Induced Oblique Shock-Wave Distortion, AIAA Journal, Vol. 35, No. 1, pp. 209-211, 1997.
11. Schlechtriem, S., Lotzerich, M., Breakdown of Tip Leakage Vortices in Compressors at Flow Conditions Close to Stall, ASME Paper No. 97-GT-41, 1997.
12. Shabbir, A., Celestina, M.L., Adamczyk, J.J., and Strazisar, A.J., The effect of Hub Leakage on 2 High Speed Axial Flow Compressor Rotors, ASME Paper 97-GT-346, 1997.
13. Smart, M.K., Kalkhoran, I.M., Popovic, S., Some aspects of streamwise vortex behavior during oblique shock wave/vortex interaction, Shock Waves, Vol. 8, pp. 243-255, 1998.
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