DocumentCode
3231046
Title
Phase measurements with reduced sensitivity of a supersonic shock flow by two-wavelength dual hologram shearing interference technique
Author
Toker, Gregory ; Levin, Daniel ; Lessin, Alexander
Author_Institution
Fac. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
fYear
1997
fDate
29 Sep-2 Oct 1997
Firstpage
313
Lastpage
321
Abstract
A novel two-wavelength technique has been applied to holographic shearing interferometry of shock wave flows around sharp and blunt nose cone models in a supersonic wind tunnel. The technique with reduced sensitivity and practically full compensation for optical aberrations, makes it possible to eliminate the difficulties of interference analysis of areas where step discontinuities in the density gradients occur. Such a case takes place in the region near the bow shock. Reconstructed lateral shearing interferograms with reduced sensitivity having a maximal fringe shift less than unity, could be used to conduct simplified numerical analysis of the density gradient distribution in the vicinity of the nose of models, without any complementary assumptions
Keywords
aerodynamics; holographic interferometry; phase measurement; shear flow; supersonic flow; wind tunnels; bow shock; density gradient distribution; density gradients; interference analysis; lateral shearing interferograms; maximal fringe shift; nose cone models; optical aberrations; phase measurements; shearing interference technique; supersonic shock flow; two-wavelength dual hologram; wind tunnel; Electric shock; Holographic optical components; Holography; Interference elimination; Nose; Optical interferometry; Optical sensors; Phase measurement; Shearing; Shock waves;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 1997. ICIASF '97 Record., International Congress on
Conference_Location
Pacific Grove, CA
Print_ISBN
0-7803-4167-8
Type
conf
DOI
10.1109/ICIASF.1997.644694
Filename
644694
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