An Investigation of Separated Flows - Part I: The Pressure Field

[1]  Glick.  Interaction of electromagnetic waves with the plasmas of hypersonic flows , 1962 .

[2]  R. Lehnert.  Correlation of Base Pressure and Wake Structure of Sharp- and Blunt-Nose Cones with Reynolds Number Based on Boundary-Layer Momentum Thickness , 1959 .

[3]  A. F. Charwat,et al.  An Investigation of Separated Flows- Part I I : Flow in the Cavity and Heat Transfer , 1961 .

[4]  James L. Amick.  A Semiempirical Relation for Laminar Separation , 1959 .

[5]  S. Feldman.  Numerical Comparison Between Exact and Approximate Theories of Hypersonic Inviscid Flow Past Slender Blunt Nosed Bodies , 1960 .

[6]  W. A. Mair.  LXVIII. Experiments on separation of boundary layers on probes in front of blunt-nosed bodies in a supersonic air stream , 1952 .

[7]  Eugene S. Love,et al.  The Base Pressure at Supersonic Speeds on Two-Dimensional Airfoils and Bodies of Revolution (With and Without Fins) Having Turbulent Boundary Layers , 1953 .

[8]  J. C. Jaeger,et al.  Conduction of Heat in Solids , 1952 .

[9]  Melvin Epstein,et al.  On the Solution of the Laminar Boundary-Layer Equations , 1959 .

[10]  Dean R Chapman,et al.  Laminar mixing of a compressible fluid , 1949 .

[11]  Luigi Crocco,et al.  A Mixing Theory for the Interaction between Dissipative Flows and Nearly-Isentropic Streams , 1952 .

[12]  Dean R. Chapman,et al.  Investigation of separated flows in supersonic and subsonic streams with emphasis on the effect of transition , 1958 .

[13]  A. Charwat.  A Modified Model of the Supersonic Laminar Wake , 1958 .

[14]  C. E. Kepler,et al.  SEPARATION OF A SUPERSONIC TURBULENT BOUNDARY LAYER , 1955 .