Higher approximations in boundary-layer theory Part 2. Application to leading edges
- 1 September 1962
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 14 (04), 481-495
- https://doi.org/10.1017/s0022112062001391
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.Keywords
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