A Subsonic Panel Method for Iterative Design of Complex Aircraft Configurations
- 1 October 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (10) , 820-825
- https://doi.org/10.2514/3.61563
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
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- An improved higher order panel method for linearized supersonic flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1978
- Inverse Method for the Design of Multielement High-Lift SystemsJournal of Aircraft, 1976
- Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex ConfigurationsAIAA Journal, 1975
- A rapid computer aided transonic airfoil design methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Calculation of Potential Flow About Arbitrary Three-Dimensional Lifting BodiesPublished by Defense Technical Information Center (DTIC) ,1972