Positive Tail Loads for Minimum Induced Drag of Subsonic Aircraft
- 1 December 1978
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 15 (12) , 837-842
- https://doi.org/10.2514/3.58457
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- Ideal Tail Load for Minimum Aircraft DragJournal of Aircraft, 1978
- Trimmed drag considerationsJournal of Aircraft, 1977
- Some Trim Drag Considerations for Maneuvering AircraftJournal of Aircraft, 1971
- Aerodynamic TheoryPublished by Springer Nature ,1934