ASYMPTOTIC THEORY OF AN UNSEPARATED SUPERSONIC TURBULENT BOUNDARY LAYER AT A COMPRESSION CORNER.
Author | : SHREEKANT AGRAWAL |
Publisher | : |
Total Pages | : 187 |
Release | : 1983 |
ISBN-10 | : OCLC:68293706 |
ISBN-13 | : |
Rating | : 4/5 (06 Downloads) |
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.