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Proceedings Paper

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

Paper Details

Date Published: 1 January 1991
PDF: 7 pages
Proc. SPIE 1332, Optical Testing and Metrology III: Recent Advances in Industrial Optical Inspection, (1 January 1991); doi: 10.1117/12.51125
Show Author Affiliations
Grigory Adamovsky, NASA/Lewis Research Ctr. (United States)
John G. Eustace, John Carroll Univ. (United States)


Published in SPIE Proceedings Vol. 1332:
Optical Testing and Metrology III: Recent Advances in Industrial Optical Inspection
Chander Prakash Grover, Editor(s)

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