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- W2013316730 abstract "An experimental study of the interaction between a shock wave and a supersonic shear layer was performed to investigate a possible shockinduced mixing enhancement effect. Hydrogen was injected parallel to the center line of the combustion chamber through holes at the base of a symmetric wedge into a Mach 2.0 air stream. The wedge was centered as a strut in the twodimensional model chamber. A wedge located at the upper plate of the chamber was used to generate an oblique shock wave that impinges on the mixing layer. Several measurement techniques like Schlieren flow visualization, Pitot tube measurements, Rayleigh Scattering and planar Laser Induced C>2 Fluorescence were applied. The results indicate that pronounced spreading of the shear layer occur downstream of the shock/shear layer interaction region. To determine the mechanism of this observed process and the extent of the increase in mixing efficiency further experimental work has to be done." @default.
- W2013316730 created "2016-06-24" @default.
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- W2013316730 date "1997-01-06" @default.
- W2013316730 modified "2023-10-16" @default.
- W2013316730 title "Interaction of a compressible shear layer with shock waves - An experimental study" @default.
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- W2013316730 doi "https://doi.org/10.2514/6.1997-392" @default.
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