Direct-inverse transonic wing-design method in curvilinear coordinates including viscous interaction
- 1 December 1991
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 28 (12) , 803-804
- https://doi.org/10.2514/3.46101
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Transonic wing design using inverse methods in curvilinear coordinatesJournal of Aircraft, 1988
- Viscous-Inviscid Interaction for Transonic Wing-Body Configurations Including Wake EffectsAIAA Journal, 1982