Prediction of Subsonic Aerodynamic Characteristics: A Case for Low-Order Panel Methods
- 1 February 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (2) , 157-163
- https://doi.org/10.2514/3.57369
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Calculation of transonic flow by means of a shock-capturing field panel methodPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Steady and Oscillatory Subsonic and Supersonic Aerodynamics around Complex ConfigurationsAIAA Journal, 1975
- Advanced panel-type influence coefficient methods applied to subsonic flowsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975