Parametric aerodynamic study of Blended-Wing-Body platforms at low subsonic speeds for UAV applications
Author:
Affiliation:
1. Aristotle University of Thessaloniki
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-3737
Reference28 articles.
1. Design of the Blended Wing Body Subsonic Transport
2. Conceptual design and analysis of blended-wing-body aircraft
3. Study of the effects of wing sweep on the aerodynamic performance of a blended wing body aircraft
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