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A new approach to the solution of the boundary layer equations of an ideal compressible flow over a flat plate

Published online by Cambridge University Press:  04 July 2016

A. Yakhot ,
G. Ben-Dor ,
Z. Rakib  and
O. Igra
A. Yakhot
Affiliation:
Department of Mechanical Engineering, Ben-Gurion University of Negev, Beer Sheva, Israel
G. Ben-Dor
Affiliation:
Department of Mechanical Engineering, Ben-Gurion University of Negev, Beer Sheva, Israel
Z. Rakib
Affiliation:
Department of Mechanical Engineering, Ben-Gurion University of Negev, Beer Sheva, Israel
O. Igra
Affiliation:
Department of Mechanical Engineering, Ben-Gurion University of Negev, Beer Sheva, Israel
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Extract

The problem of finding the temperature and velocity distribution inside the boundary layer of a compressible flow over a flat plate is a well-known problem which has been discussed by many distinguished investigators in the past five decades.

Excellent reviews of the work done on this classical hydrodynamic problem are available, for example, in the monographs of Schlichting, Loitsyanskii and Stewartson.

Type
Research Article
Information
The Aeronautical Journal , Volume 85 , Issue 840 , January 1981 , pp. 34 - 35
Copyright
Copyright © Royal Aeronautical Society 1981 

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References

1. Schlichting, H. Boundary Layer Theory, McGraw Hill 1960.Google Scholar
2. Loitsyanskii, L. G. Mechanics of liquids and gases. Int Ser of Monographs in Aeronautics & Astronautics, Pergamon Press, 1969.Google Scholar
3. Stewartson, K. The theory of laminar boundary layers in compressible fluids. Oxford Mathematical Monographs, Oxford University Press, 1964.Google Scholar
4. Emmons, H. W. and Brainerd, G. J. J. Applied Mechanics, Vol 8, pp A–105 to A-110, 1941.Google Scholar
5. Topfer, C. ZMP, Vol 60, p 397,1912.Google Scholar