Transonic Rotational Flow Around a Convex Corner.
Abstract
Results and conclusions are presented for the following problem: The development of a systematic method of solution for rotational inviscid transonic corner flows where the entropy gradient at the wall may have an arbitrary order of magnitude; The application of the method to the transonic part of a supersonic boundary layer turning a sharp corner, including both two dimensional and axially symmetric cases. (Author)
Document Details
- Document Type
- Technical Report
- Publication Date
- Sep 30, 1970
- Accession Number
- AD0715739
Entities
People
- Thomas C. Adamson Jr.
Organizations
- University of Michigan