Download or read book ASYMPTOTIC THEORY OF AN UNSEPARATED SUPERSONIC TURBULENT BOUNDARY LAYER AT A COMPRESSION CORNER. written by SHREEKANT AGRAWAL and published by . This book was released on 1983 with total page 187 pages. Available in PDF, EPUB and Kindle. Book excerpt: transverse length scale equal to the boundary-layer thickness, inviscid-flow solutions are derived in a supersonic, a hypersonic, and a transonic small-disturbance limit. Additional intermediate inviscid-flow solutions are derived in supersonic and transonic limits in order to describe the flow field at smaller distances from the corner.