Modifying a general aviation airfoil for supercritical flight

Publisher Website

1 April 1983

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

Vol. 20 (4) , 377-379
https://doi.org/10.2514/3.44879

Abstract

No abstract available

Keywords

This publication has 5 references indexed in Scilit:

AN EFFECTIVE METHOD FOR SHOCK-FREE WING DESIGN
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
A cost-effective method for shock-free supercritical wing design
Published by American Institute of Aeronautics and Astronautics (AIAA) ,1981
Shock-Free Wing Design
AIAA Journal, 1980
New Method for Designing Shock-Free Transonic Configurations
AIAA Journal, 1979
On the non‐existence of continuous transonic flows past profiles I
Communications on Pure and Applied Mathematics, 1956