The Structure of Shock Wave-Boundary Layer Interactions in Transonic Flow

  • T. C. AdamsonJr.
Conference paper
Part of the International Union of Theoretical and Applied Mechanics book series (IUTAM)

Summary

The structure of transonic shock wave-boundary layer interactions is studied using asymptotic analyses, for an oblique shock impinging on a flat plate boundary layer. Solutions for unseparated laminar and turbulent boundary layers are reviewed, and incipient separation of a turbulent boundary layer is considered.

Keywords

Univer Exter 

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References

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Copyright information

© Springer-Verlag, Berlin/Heidelberg 1976

Authors and Affiliations

  • T. C. AdamsonJr.
    • 1
  1. 1.Department of Aerospace EngineeringThe University of MichiganMichiganUSA

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