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

Grigory Adamovsky | Zendy; John Eustace | Zendy

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

Author(s) -

Grigory Adamovsky,

John Eustace

Publication year - 1991

Publication title -

proceedings of spie, the international society for optical engineering/proceedings of spie

Language(s) - English

Resource type - Conference proceedings

SCImago Journal Rank - 0.192

H-Index - 176

eISSN - 1996-756X

pISSN - 0277-786X

DOI - 10.1117/12.51125

Subject(s) - supersonic speed , position (finance) , shock (circulatory) , aerospace engineering , aerospace , computer science , bow shock (aerodynamics) , choked flow , shock wave , electric shock , mechanics , physics , engineering , mechanical engineering , medicine , finance , economics

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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