Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of Attack

E. R. VAN DRIEST

doi:10.2514/8.2149

Turbulent Boundary Layer on a Cone in a Supersonic Flow at Zero Angle of Attack

Journal of the Aeronautical Sciences (Institute of the Aeronautical Sciences) ◽

10.2514/8.2149 ◽

1952 ◽

Vol 19 (1) ◽

pp. 55-57 ◽

Cited By ~ 35

Author(s):

E. R. VAN DRIEST

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Angle Of Attack

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Finite-difference analysis of the three-dimensional turbulent boundary layer on a sharp cone at angle of attack in a supersonic flow

10.2514/6.1972-186 ◽

1972 ◽

Cited By ~ 6

Author(s):

J. ADAMS, JR.

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Finite Difference ◽

Turbulent Boundary Layer ◽

Angle Of Attack ◽

Three Dimensional ◽

Difference Analysis ◽

Finite Difference Analysis ◽

Sharp Cone

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Influence of the angle of attack on the transition from a laminar to a turbulent boundary layer in the case of supersonic flow past sharp circular cones

Fluid Dynamics ◽

10.1007/bf01090036 ◽

1983 ◽

Vol 17 (4) ◽

pp. 622-625

Author(s):

A. Ya. Yushin

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Angle Of Attack ◽

Flow Past

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ON THE EXISTENCE OF THE FIRST INTEGRAL IN THE PROBLEM OF TURBULENT BOUNDARY LAYER OPTIMAL CONTROL IN SUPERSONIC FLOW

TsAGI Science Journal ◽

10.1615/tsagiscij.2012005278 ◽

2012 ◽

Vol 43 (1) ◽

pp. 79-86

Author(s):

Kavas Garayevich Garayev

Keyword(s):

Boundary Layer ◽

Optimal Control ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

First Integral

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Transonic Shock-Turbulent Boundary Layer Interactions on Spinning Axisymmetric Bodies at Zero Angle of Attack

10.21236/ada123389 ◽

1983 ◽

Cited By ~ 1

Author(s):

George R. Inger

Keyword(s):

Boundary Layer ◽

Turbulent Boundary Layer ◽

Angle Of Attack ◽

Transonic Shock ◽

Axisymmetric Bodies

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Determination of the heat transfer properties of a turbulent boundary layer in the case of supersonic flow when the temperature distribution along the constraining wall is arbitrarily assigned

50 Jahre Grenzschichtforschung ◽

10.1007/978-3-663-20219-6_35 ◽

1955 ◽

pp. 364-384 ◽

Cited By ~ 2

Author(s):

Carlo Ferrari

Keyword(s):

Heat Transfer ◽

Boundary Layer ◽

Temperature Distribution ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Transfer Properties

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Visualization of curved swept shock wave/turbulent boundary layer interaction in supersonic flow

Journal of Visualization ◽

10.1007/s12650-020-00692-5 ◽

2020 ◽

Author(s):

Yue Zhang ◽

Liang Chen ◽

Hui-jun Tan ◽

Chao Wang ◽

Fei Cheng ◽

...

Keyword(s):

Boundary Layer ◽

Shock Wave ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Layer Interaction ◽

Boundary Layer Interaction

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A correlation technique for predicting attached turbulent boundary layer/flap interaction pressuresin supersonic flow

10.2514/6.1979-141 ◽

1979 ◽

Author(s):

R. ROSEN ◽

D. PAVISH ◽

W. ANDERSON

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Correlation Technique

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Approximate calculation of the critical pressures for turbulent boundary layer separation and attachment in supersonic flow

Fluid Dynamics ◽

10.1007/bf01019198 ◽

1972 ◽

Vol 3 (4) ◽

pp. 68-71 ◽

Cited By ~ 1

Author(s):

L. V. Gogish

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Turbulent Boundary Layer ◽

Approximate Calculation ◽

Boundary Layer Separation ◽

Layer Separation

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Numerical investigation of boundary-layer instabilities over a blunt flat plate at angle of attack in supersonic flow

Notes on Numerical Fluid Mechanics (NNFM) - New Results in Numerical and Experimental Fluid Mechanics ◽

10.1007/978-3-322-86573-1_13 ◽

1997 ◽

pp. 103-110 ◽

Cited By ~ 3

Author(s):

Guido Dietz ◽

Alexander Meijering

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Flat Plate ◽

Numerical Investigation ◽

Angle Of Attack

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On Laminar and Turbulent Boundary Layer in Supersonic Flow

Reviews of Modern Physics ◽

10.1103/revmodphys.21.510 ◽

1949 ◽

Vol 21 (3) ◽

pp. 510-515 ◽

Cited By ~ 3

Author(s):

R. Ladenburg ◽

D. Bershader

Keyword(s):

Boundary Layer ◽

Supersonic Flow ◽

Turbulent Boundary Layer

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