Computation of vortex flow around a canard/delta combination

Publisher Website

1 November 1984

journal article
Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft

Vol. 21 (11) , 858-865
https://doi.org/10.2514/3.45055

Abstract

No abstract available

Keywords

This publication has 2 references indexed in Scilit:

Damped Euler-equation method to compute transonic flow around wing-body combinations
AIAA Journal, 1982
Generation of boundary-conforming grids around wing-body configurations using transfinite interpolation
AIAA Journal, 1982