Three-dimensional boundary-layer transition on a cone at Mach 3.5

Author:

King R. A.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Reference28 articles.

1. Adams, J. C. Jr. 1971: Three-dimensional laminar boundary-layer analysis of upwash patterns and entrained vortex formation on sharp cones at angle of attack. AEDC-TR-71-215

2. Beckwith, I. E.; Creel, T. R. Jr.; Chen, F.-J.; Kendall, J. M. 1983: Freestream noise and transition measurements on a cone in a Mach 3.5 Pilot Quiet Tunnel. AIAA Paper 83-0042

3. Chapman, G. T. 1961: Some effects of leading edge sweep on boundary-layer transition at supersonic speeds. NASA TN D-1075

4. Chen, F.-J.; Malik, M. R.; Beckwith, I. E. 1989: Boundary-layer transition on a cone and flat plate at Mach 3.5. AIAA J. 27, 687–693

5. Dajeh, D. A. 1988: Stability of a supersonic boundary layer on a sharp cone at a small angle of attack. Ph.D. Dissertation, The University of Oklahoma

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