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Raman measurements of supersonic hydrogen/air mixing

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Abstract

The investigation of fuel/air mixing in high velocity compressible flow is important for a complete understanding of fluid dynamic and for engine development of a future space transportation vehicle with subsonic (ramjet) or supersonic (scramjet) combustion. Numerous configurations with parallel, transverse and oblique fuel injection through walls, ramps or struts have already been investigated[1-5].

© 1998 Optical Society of America

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