FLOW AROUND A CORNER FOR AIR IN EQUILIBRIUM (PRANDTL-MEYER EXPANSION),
Abstract
The document contains a theoretical treatment of the supersonic flow of air around a corner, using the assumptions made by Prandtl and develped by Meyer.
Document Details
- Document Type
- Technical Report
- Publication Date
- Oct 27, 1960
- Accession Number
- AD0677094
Entities
People
- L. D'attorre
Organizations
- General Dynamics