Subsonic VSTOL Aircraft Configurations with Tandem Wings
- 1 September 1979
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 16 (9) , 605-611
- https://doi.org/10.2514/3.58574
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Positive Tail Loads for Minimum Induced Drag of Subsonic AircraftJournal of Aircraft, 1978