A comparison of planar and conical boundary layer stability and transition at a Mach number of 8
暂无分享,去创建一个
Roger L. Kimmel | Kenneth F. Stetson | R. Kimmel | K. Stetson | L. Siler | J. Donaldson | L. Siler | J. Donaldson
[1] A. Demetriades. Growth of disturbances in a laminar boundary layer at Mach 3 , 1989 .
[2] M. Malik. Prediction and control of transition in supersonic and hypersonic boundary layers , 1989 .
[3] Dean R. Chapman,et al. Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature , 1949 .
[4] L. Mack. Linear Stability Theory and the Problem of Supersonic Boundary- Layer Transition , 1975 .
[5] J. Leith Potter,et al. Boundary-Layer Transition on Supersonic Cones in an Aeroballistic Range , 1974 .
[6] J. Laufer,et al. Stability and transition of a supersonic laminar boundary layer on an insulated flat plate , 1960, Journal of Fluid Mechanics.
[7] S. Pate,et al. Measurements and Correlations of Transition Reynolds Numbers on Sharp Slender Cones at High Speeds , 1971 .