Prandtl's biplane theory applied to canard and tandem aircraft
- 1 April 1980
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 17 (4) , 233-237
- https://doi.org/10.2514/3.44653
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Positive Tail Loads for Minimum Induced Drag of Subsonic AircraftJournal of Aircraft, 1978
- Minimum Trimmed Drag and Optimum c.g. PositionJournal of Aircraft, 1978
- Ideal Tail Load for Minimum Aircraft DragJournal of Aircraft, 1978
- Aerodynamic TheoryPublished by Springer Nature ,1934