Effect of wing/canard interference on the loading of a delta wing
- 1 January 1988
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 25 (1) , 18-24
- https://doi.org/10.2514/3.45535
Abstract
No abstract availableKeywords
This publication has 2 references indexed in Scilit:
- Vortex trajectories and breakdown on wing-canard configurationsJournal of Aircraft, 1985
- Effect of Leading-Edge Separation on the Lift of a Delta WingJournal of the Aeronautical Sciences, 1954