Analysis of the Twin-Fuselage Configuration and its H-Cabin Derivative
- 21 June 2003
- conference paper
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA's 3rd Annual Aviation Technology, Integration, and Operations (ATIO) Forum
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- Aerodynamic Performance of Wing-Body Configurations and the Flying WingPublished by SAE International ,1991