Observations of supersonic flat plate wake transition

AIAA Journal

Volumn 36, Issue 7, 1998, Pages 1328-1330

  Clemens, N T ^a,b   Smith, M F ^a  

^a UNIVERSITY OF TEXAS AT AUSTIN   (United States)

^b AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0005948746     PISSN: 00011452     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.520     Document Type: Article

References (7)

1. Chen, J. H., Cantwell, B. J., and Mansour, N. N., "The Effect of Mach Number on the Stability of a Plane Supersonic Wake," Physics of Fluids A, Vol. 2, No. 6, 1990, pp. 984-1004.
2. Meiburg, E., and Lasheras. J., "Experimental and Numerical Investigation of the Three-Dimensional Transition in Plane Wakes," Journal of Fluid Mechanics, Vol. 190, 1988, pp. 1-37.
3. Clemens, N. T, Smith, M. F., and Fernandez, J. V, "Observations of Supersonic Flat Plate Wake Transition," AIAA Paper 96-0785, Jan. 1996.
4. Smith, K. M., and Dutton, J. C., "Large-Scale Structures in Supersonic Reattaching Shear Flows," AIAA Paper 95-2251, June 1995.
5. Alvi, F. S., Krothapalli, A., and Washington, D., "Fluctuating Pressure Measurements in a Highly Compressible Countercurrent Turbulent Shear Layer," AIAA Paper 95-2175, Jan. 1995.
6. Vreman, B., Kuerten, H., and Geurts, B., "Shocks in DNS of the Three-Dimensional Mixing Layer," Proceedings of the Tenth Symposium on Turbulent Shear Flows, Pennsylvania State Univ., 1995.
7. Dimotakis, P. E., "Turbulent Free Shear Layer Mixing and Combustion," High-Speed Flight Propulsion Systems, edited by S. N. B. Murthy and E. T. Curran, Vol. 137, Progress in Astronautics and Aeronautics, AIAA, Washington, DC, 1991, pp. 265-340.