High-enthalpy shock/boundary-layer interaction on a double wedge

High-enthalpy shock/boundary-layer interaction on a double wedge

Interaction between a shock wave and a boundary layer at a compression corner can produce a region of separated flow. The length of separation is important in determining aerodynamic forces, and the heat transfer at reattachment is important for the design of thermal protection systems. The effects...

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Bibliographic Details
Main Author: Davis, Jean-Paul
Format: Others
Published: 1999
Online Access:https://thesis.library.caltech.edu/788/1/Davis_jp_1999.pdf
Davis, Jean-Paul (1999) High-enthalpy shock/boundary-layer interaction on a double wedge. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/4C98-MN23. https://resolver.caltech.edu/CaltechETD:etd-02272008-125333 <https://resolver.caltech.edu/CaltechETD:etd-02272008-125333>

Internet

https://thesis.library.caltech.edu/788/1/Davis_jp_1999.pdf
Davis, Jean-Paul (1999) High-enthalpy shock/boundary-layer interaction on a double wedge. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/4C98-MN23. https://resolver.caltech.edu/CaltechETD:etd-02272008-125333 <https://resolver.caltech.edu/CaltechETD:etd-02272008-125333>

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