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

Grigory Adamovsky; John G. Eustace

doi:10.1117/12.51125

1 January 1991 Optical techniques for determination of normal shock position in supersonic flows for aerospace applications

Grigory Adamovsky, John G. Eustace

Author Affiliations +

Proceedings Volume 1332, Optical Testing and Metrology III: Recent Advances in Industrial Optical Inspection; (1991) https://doi.org/10.1117/12.51125
Event: 34th Annual International Technical Symposium on Optical and Optoelectronic Applied Science and Engineering, 1990, San Diego, CA, United States

Abstract

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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Grigory Adamovsky and John G. Eustace "Optical techniques for determination of normal shock position in supersonic flows for aerospace applications", Proc. SPIE 1332, Optical Testing and Metrology III: Recent Advances in Industrial Optical Inspection, (1 January 1991); https://doi.org/10.1117/12.51125

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