Instability of Hypersonic Flow Past Blunt Cones - Effects of Mean Flow Variations -

[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.