An interactive three-dimensional boundary-layer method for transonicflow over swept wings

Publisher Website

9 January 1989

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

https://doi.org/10.2514/6.1989-112

Abstract

No abstract available

This publication has 2 references indexed in Scilit:

Nonuniform grid method for turbulent boundary layers
Published by Springer Nature ,2005
A Three-Dimensional Boundary-Layer Method for Flow over Delta Wings with Leading-Edge Separation
Published by SAE International ,1985