Effects of Periodic Unsteady Wake Flow and Pressure Gradient on Boundary Layer Transition Along the Concave Surface of a Curved Plate

M. T. Schobeiri, R. E. Radke
1994 Volume 1: Turbomachinery   unpublished
doi:10.1115/94-gt-327 fatcat:nfyycy5bgjbdth3uxmdwgvylbu