An inverse boundary element method for single component airfoil design
- 1 June 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (6) , 541-543
- https://doi.org/10.2514/3.45162
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- A Potential Flow Design Method for Multicomponent Airfoil SectionsJournal of Aircraft, 1978
- Multiple element airfoils optimized for maximum lift coefficient.AIAA Journal, 1972