Application of Optical Measurement Techniques to Supersonic and Hypersonic Aerospace Flows
Publication: Journal of Aerospace Engineering
Volume 22, Issue 4
Abstract
Experimental investigation is essential to improve the understanding of aerospace flows. During the last years, effort has been put on the development of optical diagnostics capable of imaging or yielding data from the flow in a nonintrusive way. The application of some of these techniques to supersonic and hypersonic flows can be highly challenging due to the high velocity, strong gradients, and restricted optical access generally encountered. Widely used qualitative and semiquantitative optical flow diagnostics are shadowgraph, schlieren, and interferometry. Laser-based techniques such as laser Doppler anemometry and particle image velocimetry are well established for investigation of supersonic flows, but as yet their use in hypersonic flows has been limited. Other relevant measurement techniques include particle tracking velocimetry, Doppler global velocimetry, laser-two-focus anemometry, background oriented schlieren and laser induced fluorescence methods. This paper reviews the development of these and further optical measurement techniques and their application to supersonic and hypersonic aerospace flows in recent years.
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Information
Published In
Journal of Aerospace Engineering
Volume 22 • Issue 4 • October 2009
Pages: 383 - 395
Copyright
© 2009 ASCE.
History
Received: Nov 7, 2007
Accepted: Sep 26, 2008
Published online: Sep 15, 2009
Published in print: Oct 2009
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