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Comparison of Reacting and Non-reacting Shear Layers at a High Subsonic Mach Number

C. T. Chang

出版	National Aeronautics and Space Administration, 1993
URL	http://books.google.com.hk/books?id=qaM3AQAAMAAJ&hl=&source=gbs_api

註釋

The flow field in a hydrogen-fueled planar reacting shear layer was measured with an LDV system and is compared with a similar air to air case without combustion. Measurements were made with a speed ratio of 0.34 with the highspeed stream at Mach 0.71. They show that the shear layer with reaction grows faster than one without, and both cases are within the range of data scatter presented by the established database. The coupling between the streamwise and the cross-stream turbulence components inside the shear layer is slow, and reaction only increased it slightly. However, a more organized pattern of the Reynolds stress is present in the reacting shear layer, possibly as a result of larger scale structure formation in the layer associated with heat release.