COMPUTATION of SEPARATION AHEAD of BLUNT FIN in SUPERSONIC TURBULENT FLOW
Reference12 articles.
1. Kaufman, L.G., Korkegi, R.H., and Morton, L.C., “Shock Impingement Caused by Boundary Layer Separation Ahead of Blunt Fin,” ARL 72-0118, 1972, Wright-Patterson Air Force Base, Ohio.
2. “Blunt Fin-Induced Shock Wave/ Turbulent Boundary Layer Interaction,”;Dolling;AIAA J.,1982
3. “Simulation of Blunt-Fin-Induced Shock Wave and Turbulent Boundary-Layer Interaction,”;Hung;J. Fluid Mechanics,1985
4. Rodi, P. E. and Dolling, D. S., ” Experimental Study of the Effects of Leading Edge Geometry on Fin Induced Turbulent Separated Flow at Mach 5: Preliminary Results,” AIAA Paper 86–0344, Jan. 1986.
5. Baldwin, B.S. and Lomax, H., “Thin-Layer Approximation and Algebraic Model for Separated Turbulent Flows,” AIAA paper 78–257, Jan. 1978.