Laminar boundary layer oblique shock wave interaction on flat and curved plates

Author:

Greber Isaac,Hakkinen Raimo J.,Trilling Leon

Publisher

Springer Science and Business Media LLC

Subject

Applied Mathematics,General Physics and Astronomy,General Mathematics

Reference8 articles.

1. F. W. Barry,A. H. Shapiro, andE. P. Neumann,The Interaction of Shock Waves with Boundary Layers on a Flat Surface, M.I.T. Meteor Report 52 (1950).

2. L. Trilling andR. J. Hakkinen,The Calibration of the Stanton Tube as a Skin Friction Meter, 50 Jahre Grenzschichtforschung, pp. 201–209 (1955).

3. S. S. Abarbanel,The Calibration of the Stanton Tube as a Skin Friction Meter, M. S. Thesis, M.I.T. (May 1955).

4. Dean R. Chapman,Donald M. Kuehn, andHoward K. Larson,Investigation of Separated Flows in Supersonic and Subsonic Streams with Emphasis on the Effect of Transition, NACA TN 3869 (1957).

5. G. E. Gadd,Interactions Between Wholly Laminar or Wholly Turbulent Boundary Layers and Shock Waves Strong Enough to Cause Separation, J. aeron. Sci.5 (11), 20 (1953).

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1. WP-1 Reference Cases of Laminar and Turbulent Interactions;Notes on Numerical Fluid Mechanics and Multidisciplinary Design;2020-07-31

2. Study of Shock Wave Boundary Layer Interaction in Hypersonic Flows Using Various Turbulence Models;Advances in Mechanical Engineering;2020-06-30

3. Laminar Shock/Boundary-Layer Interaction — A Numerical Test Problem;Numerical Treatment of the Navier-Stokes Equations;1990

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