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Optical techniques for determination of normal shock position in supersonic flows for aerospace applicationsTechniques 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.
Document ID
19900016007
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Adamovsky, Grigory (NASA Lewis Research Center Cleveland, OH., United States)
Eustace, John G. (John Carroll Univ. Cleveland, OH., United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1990
Subject Category
Instrumentation And Photography
Report/Patent Number
E-5599
NASA-TM-103201
NAS 1.15:103201
Meeting Information
Meeting: Conference on Optical Testing and Metrology
Location: San Diego, CA
Country: United States
Start Date: July 8, 1990
End Date: July 13, 1990
Sponsors: Society of Photo-Optical Instrumentation Engineers
Accession Number
90N25323
Funding Number(s)
PROJECT: RTOP 505-62-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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