Title :
Experimental investigation of supersonic/hypersonic flow fields based on a new approach using holographic optical techniques
Author :
Toker, G. ; Levin, D. ; Stricker, J.
Author_Institution :
Dept. of Aerosp. Eng., Technion-Israel Inst. of Technol., Haifa, Israel
Abstract :
This paper describes a holographic approach designed to provide a comprehensive acquisition of the optical information obtained from supersonic/hypersonic flow fields. A simultaneous application of three holographic diagnostic techniques, namely, schlieren- and shadowgraphy, moire deflectometry and interferometry, yields a more accurate measurement of the density distribution in complex compressible flow fields. The holographic approach makes it possible to increase the sensitivity of the interferometric measurements with compensation of the optical aberration to suit the low density field of hypersonic flows. Preliminary experiments with the new approach rendered satisfactory results, proving the potential use of these techniques
Keywords :
aberrations; aerodynamics; compressible flow; flow measurement; holographic interferometry; hypersonic flow; moire fringes; schlieren systems; supersonic flow; wind tunnels; aerodynamics; complex compressible flow fields; density distribution; diagnostic techniques; holographic optical techniques; hypersonic flow fields; interferometry; low density field; moire deflectometry; optical aberration; schlieren systems; shadowgraphy; supersonic flow fields; wind tunnels; High speed optical techniques; Holographic optical components; Holography; Image motion analysis; Optical distortion; Optical filters; Optical interferometry; Optical refraction; Optical sensors; Optical variables control;
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1995. ICIASF '95 Record., International Congress on
Conference_Location :
Wright-Patterson AFB, OH
Print_ISBN :
0-7803-2088-3
DOI :
10.1109/ICIASF.1995.519116