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Higher approximations in boundary-layer theory Part 2. Application to leading edges

Published online by Cambridge University Press:  28 March 2006

Milton Van Dyke
Milton Van Dyke
Affiliation:
Department of Aeronautics and Astronautics, Stanford University
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Abstract

The general analysis of Part 1 is applied to the calculation of the second-order viscous and thermal boundary layers for the axisymmetric stagnation point, unsymmetric plane stagnation point, and cusped leading edge at ideal incidence. The second-order effect upon heat transfer is found usually to be of the order of one-third of that for skin friction.

Type
Research Article
Information
Journal of Fluid Mechanics , Volume 14 , Issue 4 , December 1962 , pp. 481 - 495
Copyright
© 1962 Cambridge University Press

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References

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