TURBULENT BOUNDARY LAYERS IN COMPRESSIBLE FLOW ANDnTHEIR INTERACTIONS WITH NORMAL SHOCK WAVES A SURVEY AND PROPOSED INVESTIGATION

摘要

The main work on the development of compressible turbulent boundary layers has been reviewed It appears that significant gaps exist in the available data and techniques for dealing with compressible turbulent boundary layers in zero pressure gradient no detailed work has been found which relates to the shock free supersonic adverse pressure gradient case The separation of a supersonic boundary layer will probably differ markedly from that of the simpler incompressible layer