Transition of Hypersonic Boundary Layer
暂无分享,去创建一个
[1] P. S. Klebanoff,et al. The three-dimensional nature of boundary-layer instability , 1962, Journal of Fluid Mechanics.
[2] H. Nagamatsu,et al. Hypersonic Nozzle Expansion of Air With Atom Recombination Present , 1961 .
[3] H. T. Nagamatsu,et al. Hypersonic Shock Tunnel , 1959 .
[4] Ronald F. Probstein,et al. THE TRANSVERSE CURVATURE EFFECT IN COMPRESSIBLE AXIALLY-SYMMETRIC LAMINAR BOUNDARY LAYER FLOW , 1956 .
[5] R. Korkegi. Transition Studies and Skin-Friction Measurements on an Insulated Flat Plate at a Mach Number of 5.8 , 1956 .
[6] F. K. Hill. Boundary-Layer Measurements in Hypersonic Flow , 1956 .
[7] E. Winkler,et al. Experimental Investigation of Turbulent Boundary Layers in Hypersonic Flow , 1955 .
[8] H. Schlichting. Boundary Layer Theory , 1955 .
[9] L. Howarth,et al. Modern Developments in Fluid Dynamics—High Speed Flow , 1954 .
[10] Donald Coles,et al. Measurements of Turbulent Friction on a Smooth Flat Plate in Supersonic Flow , 1954 .
[11] Dean R. Chapman,et al. Measurements of Turbulent Skin Friction on Cylinders in Axial Flow at Subsonic and Supersonic Velocities , 1953 .
[12] E. R. V. Driest,et al. Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of Attack , 1952 .
[13] Robert E. Wilson,et al. Turbulent Boundary-Layer Characteristics at Supersonic Speeds-Theory and Experiment , 1950 .
[14] Dean R. Chapman,et al. Temperature and Velocity Profiles in the Compressible Laminar Boundary Layer with Arbitrary Distribution of Surface Temperature , 1949 .
[15] T. Kármán,et al. Boundary Layer in Compressible Fluids , 1938 .