Behaviour of unsteady transonic shock / boundary layer interactions with three-dimensional effects

47th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition

Volumn , Issue , 2009, Pages

  Bruce, P J K ^a   Babinsky, H ^a  

^a UNIVERSITY OF CAMBRIDGE   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

BOUNDARY LAYERS; FLOW FIELDS; HIGH SPEED PHOTOGRAPHY; LASER DOPPLER VELOCIMETERS; VISCOUS FLOW;

EXPERIMENTAL INVESTIGATIONS; LASER DOPPLER ANEMOMETRY; MEASUREMENT TECHNIQUES; PRESSURE PERTURBATION; SCHLIEREN PHOTOGRAPHY; SHOCK/BOUNDARY LAYER INTERACTIONS; THREE DIMENSIONAL EFFECT; VISCOUS BOUNDARY LAYERS;

TRANSONIC AERODYNAMICS;

EID: 78549291043     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2009-1590     Document Type: Conference Paper

References (12)

1. Sajben, M. and Bogar, TJ and Kroutil, JC, Forced oscillation experiments in supercritical diffuser flows, AIAA Journal 22, No. 4, pp465-474, 1984.
2. Ott, P. and Bolcs, A. and Fransson, T.H., Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle, Journal of Turbomachinery 117, pp106-114, 1995.
3. Handa, T. and Masuada, M. and Matsuo, K., Mechanism of Shock Wave Oscillation in Transonic Diffusers, AIAA Journal 41, No. 1, pp64-70, 2003.
4. Bur, R. and Benay, R. and Galli, A. and Berthouze, P., Experimental and numerical study of forced shock-wave oscillations in a transonic channel, Aerospace Science and Technology 10, pp265-278, 2006.
5. Bruce, P.J.K. and Babinsky, H., Unsteady shock wave dynamics, Journal of Fluid Mechanics 603, pp463-473, 2008.
6. Bruce, P.J.K. and Babinsky, H., Unsteady normal shock wave boundary layer interactions with control, AIAA Paper 2008-0721, 2008.
7. Ogawa, H. and Babinsky, H., Wind Tunnel Setup for Investigations of Normal Shock Wave/Boundary-Layer Interaction Control, AIAA Journal 44, No. 11, pp2803-2805, 2006.
8. Holden, H.A. and Babinsky, H., Effect of microvortex generators on separated normal shock/boundary layer interactions, J. Aircraft 44, No. 1, pp170-174, 2007.
9. Lin, J.C., Review of research on low-profile vortex generators to control boundary-layer separation, Progress in Aerospace Sciences 38, pp389-420, 2002.
10. Delery, J., Turbulent shock-boundary layer interaction and its control, Progress in Aerospace Sciences 22, No. 4, pp209- 280, 1985.
11. Bhanderi, H. and Babinsky, H., Improved Boundary Layer Quantities in the Shock Wave Boundary Layer Interaction Region on Bumps, AIAA Paper 2005-4896, 2005.
12. Edwards, J.A. and Squire, L.C., An experimental study of the interaction of an unsteady shock with a turbulent boundary layer, Aeronautical Journal 97, No. 970, pp337-348, 1993.