Instability of Hypersonic Flow Past Blunt Cones - Effects of Mean Flow Variations -
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[1] P. Lax. Weak solutions of nonlinear hyperbolic equations and their numerical computation , 1954 .
[2] A. Nayfeh,et al. Effect of heat transfer on the stability of compressible boundary layers , 1992 .
[3] F. Bertolotti. Linear and nonlinear stability of boundary layers with streamwise varying properties , 1991 .
[4] F. Monnoyer De Galland. Calculation of three-dimensional attached viscous flow on general configurations using second-order boundary-layer theory , 1990 .
[5] Vahid Esfahanian. Computation and stability analysis of laminar flow over a blunt cone in hypersonic flow , 1991 .
[6] M. V. Dyke,et al. Second-Order Compressible Boundary-Layer Theory with Application to Blunt Bodies in Hypersonic Flow, , 1962 .
[7] E. Reshotko,et al. Stability of the Laminar Boundary Layer on a Blunted Plate in Supersonic Flow , 1980 .
[8] K. Stetson,et al. Laminar boundary layer stability experiments on a cone at Mach 8. V - Tests with a cooled model , 1989 .
[9] M. Malik,et al. Effect of nose bluntness on boundary layer stability and transition , 1990 .
[10] Lester Lees,et al. The stability of the laminar boundary layer in a compressible fluid , 1946 .
[11] K. Stetson. Nosetip bluntness effects on cone frustum boundary layer transition in hypersonic flow , 1983 .
[12] M. Simen. COSMET - A DLR-Dornier Computer Program for Compressible Stability Analysis with Local Metric , 1991 .
[13] Daniel Arnal. Boundary layer transition: Predictions based on linear theory , 1994 .
[14] M. Lighthill. On displacement thickness , 1958, Journal of Fluid Mechanics.