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- W2080666918 abstract "The temperature distribution in the flowfield of a two-dimensional hydrogen jet in a supersonic air stream has been experimentally investigated. Hydrogen was injected parallel to the freestream air through the base of a strut centered in the combustion chamber. This strut, formed like a symmetrical wedge, also served as a flameholder. The aim of this work was the measurement of temperatures in a turbulent supersonic hydrogen-fueled ramjet for better understanding of combustion phenomena and improvement of theoretical predictions. Coherent Anti-Stokes Raman Spectroscopy (CARS) was used as a diagnostic tool for temperature mapping in the combustion chamber. Temperature profiles were determined at three different axial locations by translating the CARS probe-volume vertically across the combustor. Experimental parameters were the total inlet temperature of mainstream-air and the mass flow of injected hydrogen. Schlieren photographs and video pictures of the 306-nm-OH-intensity have been used to get a qualitative understanding of the flowfield and to determine the locations of interest for CARS measurements. Due to the nonlinear dependence of CARS on temperature and the highly turbulent flowfield, time averaging would lead to serious measurement errors. Thus, single pulse CARS measurements have been recorded using nitrogen as a probe molecule." @default.
- W2080666918 created "2016-06-24" @default.
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- W2080666918 date "1994-01-01" @default.
- W2080666918 modified "2023-09-27" @default.
- W2080666918 title "CARS TEMPERATURE MEASUREMENTS IN A SUPERSONIC RAMJET COMBUSTION CHAMBER" @default.
- W2080666918 doi "https://doi.org/10.1615/intjenergeticmaterialschemprop.v3.i1-6.140" @default.
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