INVERSE COMPUTATION OF SUPERSONIC INVISCID FLOW FIELDS WITH IMBEDDED SHOCKS: ANALYSIS AND USER'S MANUAL.
Abstract
Instructions are given for the use of a program to compute the flow field about a supersonic configuration.
Document Details
- Document Type
- Technical Report
- Publication Date
- Dec 15, 1967
- Accession Number
- AD0664938
Entities
People
- Michael Abbett