Leading Edge Bluntness And Boundary Layer Displacement Effects On Attached And Separated Laminar Boundary Layers In A Compression Corner
Download Leading Edge Bluntness And Boundary Layer Displacement Effects On Attached And Separated Laminar Boundary Layers In A Compression Corner PDF/ePub or read online books in Mobi eBooks. Click Download or Read Online button to get Leading Edge Bluntness And Boundary Layer Displacement Effects On Attached And Separated Laminar Boundary Layers In A Compression Corner book now. This website allows unlimited access to, at the time of writing, more than 1.5 million titles, including hundreds of thousands of titles in various foreign languages.
Effects of Wall Cooling and Leading-edge Blunting on Ramp-induced, Laminar Flow Separations at Mach Numbers from 3 Through 6
The effects of wall cooling and nose bluntness on laminar and transitional reattaching flows induced by a 9.5-degree ramp were investigated at Mach numbers from 3 through 6 measuring the longitudinal surface pressure and heat-transfer rate distributions, as well as the flow-field pressures, at several longitudinal stations. Reynolds number based on flat-plate length was varied from 0.25 to 1.0 million. The trend in the change in interaction length with Reynolds number increase indicated laminar reattachment at all test Reynolds numbers at M = 6 and transitional at the two higher Reynolds numbers at M = 3.