Efficient Transonic Shock-Free Wing Redesign Procedure Using a Fictitious Gas Method
- 1 February 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 18 (2) , 143-148
- https://doi.org/10.2514/3.50744
Abstract
No abstract availableThis publication has 7 references indexed in Scilit:
- Artificial compressibility methods for numerical solutions of transonic full potential equationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Supercritical Wing Sections IIIPublished by Springer Nature ,1977
- Transonic Airfoil Analysis and Design Using Cartesian CoordinatesJournal of Aircraft, 1976
- Application of Generalized Potentials on Plane Transonic FlowPublished by Springer Nature ,1976
- Iterative solution of transonic flows over airfoils and wings, including flows at mach 1Communications on Pure and Applied Mathematics, 1974
- A Finite-Difference Method for Transonic Airfoil DesignAIAA Journal, 1973
- Calculation of plane steady transonic flowsAIAA Journal, 1971