Techniques for the quantitative determination of shock position in supersonic flows using direct and indirect methods is presented. A description of an experimental setup is also presented, different configurations of shock position sensing systems are explained, and some experimental results are given. All of the methods discussed are analyzed to determine the ease of technology transfer from the laboratory to in-flight operation.


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    Title :

    Optical techniques for determination of normal shock position in supersonic flows for aerospace applications


    Contributors:

    Conference:

    Optical Testing and Metrology III: Recent Advances in Industrial Optical Inspection ; 1990 ; San Diego, CA, United States


    Publication date :

    1990-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English