Iterative three-dimensional transonic wing design using integral equations
- 1 August 1985
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 22 (8) , 655-660
- https://doi.org/10.2514/3.45182
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
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- Artificial viscosity method for the design of supercritical airfoils. [Analysis code H]Published by Office of Scientific and Technical Information (OSTI) ,1979
- Numerical Calculation of Transonic Potential Flow about Wing-Body CombinationsAIAA Journal, 1979
- Numerical calculation of the transonic flow past a swept wing. [FLO 22]Published by Office of Scientific and Technical Information (OSTI) ,1977
- Airfoil Section Drag Reduction at Transonic Speeds by Numerical OptimizationPublished by SAE International ,1976