Effect of dimples on glancing shock wave turbulent boundary layer interactions

AIAA Paper

Volumn , Issue , 2004, Pages 6544-6554

  Lada, C ^a   Amir, M ^a   Wong, C ^a   Kontis, K ^a  

^a UNIVERSITY OF MANCHESTER   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; CORRELATION METHODS; FUSELAGES; INTAKE SYSTEMS; PRESSURE DROP; TRANSONIC FLOW; VORTEX FLOW;

BOUNDARY LAYER INTERACTIONS; FLOW FIELDS; MACH NUMBER; VISCOUS FLOWS;

SHOCK WAVES;

EID: 2942702329     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. Hussain, S., Ph.D. Thesis, "A study of the interaction between a glancing shock wave and a turbulent boundary layer - The effects of leading edge bluntness and sweep" 1985.
2. Kubota, H., and Stollery, J. L., "An Experimental Study of the Interaction between a Glancing Shock Wave and a Turbulent Boundary Layer", Fluid Mechanics Journal, Vol.116, 1982, pp431-458.
3. Chokani, N., and Squire, L. C., "Transonic Shockwave / Turbulent Boundary Layer Interactions On a Porous Surface", Aeronautical Journal, Vol.97, May 1993, pp.163-170.
4. McConnell, D. A., Ph.D. Thesis, "Roughness Effects on Impinging Shock Wave / Turbulent Boundary Layer Interactions", (Churchill College Cambridge University Engineering Department) August 1999
5. Squire, L. C., "Interaction of Swept and Unswept Normal Shock Waves with Boundary Layers", AIAA Journal, Vol.34, No. 10, October 1996
6. Merzkirch, M., "Flow Visualization", Academic Press Inc. 1987
7. McLahlan, B. G., Bell, J. H., "Pressure-Sensitive Paint in Aerodynamic Testing", Experimental Thermal and Fluid Science 1995 p. 470-485
8. Wong C., Amir M., Baudoin M., Lada C., Kontis K., "Molecular Image Sensing for Pressure and Temperature Surface Mapping of Aerodynamic Flow", AIAA-2004-0598.