Analysis, Design, and Optimization of Noncylindrical Fuselage for Blended-Wing-Body Vehicle
Author:
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/1.417
Reference13 articles.
1. Blended-wing-body subsonic commercial transport
2. Airframe integration trade studies for a reusable launch vehicle
3. Pressure cabins of elliptic cross section
4. Structural Concepts Study of Non-circular Fuselage Configurations
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