A numerical study of supersonic viscous cone flow at high angle of attack

Publisher Website

26 January 1976

proceedings article
Published by American Institute of Aeronautics and Astronautics (AIAA)

https://doi.org/10.2514/6.1976-97

Abstract

No abstract available

This publication has 1 reference indexed in Scilit:

Computation of Space Shuttle Flowfields Using Noncentered Finite-Difference Schemes
AIAA Journal, 1973

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