A numerical solution of the flow field over a transonic airfoil including strong-shock-induced flow separation

Publisher Website

14 July 1976

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

https://doi.org/10.2514/6.1976-330

Abstract

No abstract available

This publication has 3 references indexed in Scilit:

Supercritical Wing Sections II
Published by Springer Nature ,1975
Iterative solution of transonic flows over airfoils and wings, including flows at mach 1
Communications on Pure and Applied Mathematics, 1974
APPLICATION OF THE GENERALIZED GALERKIN METHOD TO THE COMPUTATION OF FLUID FLOWS
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973