Effects of Mach number on turbulent separation behaviours induced by blunt fin

Experiments in Fluids

Volumn 25, Issue 4, 1998, Pages 347-351

  Wang, S F ^a   Ren, Z Y ^a   Wang, Y ^a  

^a INSTITUTE OF MECHANICS   (China)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FINS (HEAT EXCHANGE); FLOW PATTERNS; FLOW VISUALIZATION; HEAT TRANSFER; PRESSURE; SHOCK WAVES;

BLUNT FIN; MACH NUMBER; TURBULENT SEPARATION;

TURBULENT FLOW;

EID: 0032154392     PISSN: 07234864     EISSN: None     Source Type: Journal    
DOI: 10.1007/s003480050239     Document Type: Article

References (8)

1. Aso S; Kuranaga S; Hayashi M (1991) Detailed measurements on unsteady properties in three-dimensional shock/turbulent boundary layer interaction induced by blunt fin at Mach number 4. AIAA Paper 91-1755
2. Deng Xueying; Wang Yu (1991) Separation behaviours in blunt fin induced shock wave/boundary layer interactions. Proceedings of the First International Conference on Experimental Fluid Mechanics (F.G. Zhuang Eds.), Chengdu, China, 71-76
3. Dolling DS; Bogdonoff SM (1982) Blunt fin-induced shock wave/turbulent boundary layer interaction. AIAA Journal 20: 1674-1680
4. Erengil ME; Dolling DS (1992) Effects of sweepback on unsteady separation in Mach 5 compression ramp interactions. AIAA Paper 92-0430
5. Gonsalez JC; Dolling DS (1993) Correlation of interaction sweepback effects on the dynamics of shock-induced turbulent separation. AIAA Paper 93-0776
6. Price AE; Stallings RL (1967) Investigation of turbulent separated flows in the vicinity of fin type protuberances at supersonic Mach numbers. NASA TN-D 3804
7. Wang Shifen; Wang Yu (1994) A new method to obtain undistorted full-scale patter of oil flow visualization. Proceedings of the Third Asian Symposium on Visualization, Chiba, Japan, 932-937
8. Wirikelmann AE (1972) Experimental investigation of a fin protuberance partially immersed in a turbulent boundary layer at Mach 5. NOLTR-72-33