Structure of a reattaching supersonic shear layer
A Mach 1.83 fully developed turbulent boundary layer with boundary layer thickness, free stream velocity, and Reynolds number of 7.5 mm, 476 m/s, and 6.2 x 10 to the 7th/m, respectively, was separated at a 25.4-mm backward step and formed a shear layer. Fast-response pressure transducers, schlieren...
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1990
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| Online Access: | https://bspace.buid.ac.ae/handle/1234/3399 |
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