Symmetrical singularity model for lifting potential flow analysis
- 1 September 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 13 (9) , 733-734
- https://doi.org/10.2514/3.44554
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- The use of higher-order surface singularity distributions to obtain improved potential flow solutions for two-dimensional lifting airfoilsComputer Methods in Applied Mechanics and Engineering, 1975
- Advanced panel-type influence coefficient methods applied to subsonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Calculation of Potential Flow About Arbitrary Three-Dimensional Lifting BodiesPublished by Defense Technical Information Center (DTIC) ,1972