A Re-examination of the Juncture between the Sonic Line and a Shock in Flows with M < 1.
Abstract
A possibility that the flow field at the juncture of the sonic line and a shock in flows with high subsonic Mach numbers can be described by a similarity solution is examined in detail. For physical reasons singularities propagating in the supersonic region towards the point of junction are excluded. A heuristic argument is made showing why similarity solutions are unlikely. The essential features of flow patterns computed by Nocilla are described. (Modified author abstract)
Document Details
- Document Type
- Technical Report
- Publication Date
- May 01, 1973
- Accession Number
- AD0760801
Entities
People
- Karl G. Guderley
- Y. V. G. Acharya