High angle of attack inviscid flow calculations over a Shuttle-like vehicle with comparisons to flight data

Publisher Website

13 July 1983

conference paper
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1983-1798

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

Multishocked, Three-Dimensional Supersonic Flowfields with Real Gas Effects
AIAA Journal, 1973