Cant angle morphing winglets investigation for the enhancement of the aerodynamic, stability and performance characteristics of a tactical Blended-Wing-Body UAV-Reference-Cited by-同舟云学术

Cant angle morphing winglets investigation for the enhancement of the aerodynamic, stability and performance characteristics of a tactical Blended-Wing-Body UAV

Published:2022-04 Issue: Volume:123 Page:107467
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Panagiotou P.,Antoniou S.^ORCID,Yakinthos K.^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

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3. Winglet Design and Optimization for UAVs;Weierman,2010

4. A CFD-aided investigation of the morphing winglet concept for the performance optimization of fixed-wing MALE UAVs;Panagiotou,2018

5. Design of winglets for high-performance sailplanes;Maughmer;J. Aircr.,2003

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