Aerodynamic investigation of twist and cant angles for joined wing transport aircraft
- 6 January 1997
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 4 references indexed in Scilit:
- Aerodynamic - structural optimization of positive/negative stagger joined wing configurationsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Benefits of dual wings over single wings for high-performance business airplanesJournal of Aircraft, 1984
- Structural Weight Comparison of a Joined Wing and a Conventional WingJournal of Aircraft, 1982
- Subsonic VSTOL Aircraft Configurations with Tandem WingsJournal of Aircraft, 1979