Experimental Laminar Transitional And Turbulent Boundary Layer Profiles On A Wedge At Local Mach Number 6 5 And Comparisons With Theory
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Experimental Laminar, Transitional, and Turbulent Boundary-layer Profiles on a Wedge at Local Mach Number 6.5 and Comparisons with Theory
Wind tunnel investigation of laminar, transitional, and turbulent boundary layer profiles on wedge at hypersonic speed to confirm theoretical analysis.