Effect of downwash on the induced drag of canard-wing combinations
- 1 May 1982
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 19 (5) , 410-411
- https://doi.org/10.2514/3.44764
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- 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
- Ideal Tail Load for Minimum Aircraft DragJournal of Aircraft, 1978