A DOE-based method for the aerodynamic, stability and layout optimization of a tactical Blended-Wing-Body UAV
Author:
Affiliation:
1. Aristotle University of Thessaloniki
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2022-0127
Reference26 articles.
1. Design of the Blended Wing Body Subsonic Transport
2. Conceptual design of a Blended Wing Body MALE UAV
3. Airframe Design for Silent Fuel-Efficient Aircraft
4. Fire and evacuation analysis in BWB aircraft configurations: computer simulations and large-scale evacuation experiment
5. A New Structural Design Concept for Blended Wing Body Cabins
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