Compressible laminar boundary layer with heat transfer and pressure gradient

  • L. Crocco
  • C. B. Cohen


Exact solutions are obtained for Stewartson’s equations of the compressible laminar boundary layer including the effects of heat transfer and pressure gradient. Then, after formulation of an extension of Thwaites’ method to include the effects of heat transfer, the exact solutions are used to evaluate the necessary parameters of the new method.


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Copyright information

© Springer Fachmedien Wiesbaden 1955

Authors and Affiliations

  • L. Crocco
    • 1
  • C. B. Cohen
    • 1
  1. 1.Lewis Flight Propulsion LaboratoryPrinceton University, NACAUSA

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