Minimum Induced Drag of Canard Configurations
- 1 September 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (9) , 792-794
- https://doi.org/10.2514/3.61557
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- Wind-Tunnel Measurements of Wing-Canard Interference and a Comparison with Various TheoriesSAE International Journal of Advances and Current Practices in Mobility, 1981
- Prandtl's biplane theory applied to canard and tandem aircraftJournal of Aircraft, 1980
- Subsonic VSTOL Aircraft Configurations with Tandem WingsJournal of Aircraft, 1979
- Positive Tail Loads for Minimum Induced Drag of Subsonic AircraftJournal of Aircraft, 1978
- Minimum Trimmed Drag and Optimum c.g. PositionJournal of Aircraft, 1978