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CFD-aided optimization of a tactical Blended-Wing-Body UAV platform using the Taguchi method

  • Published:2021-01 Issue: Volume:108 Page:106395
  • ISSN:1270-9638
  • Container-title:Aerospace Science and Technology
  • language:en
  • Short-container-title:Aerospace Science and Technology

Author:

Kapsalis S.,Panagiotou P.,Yakinthos K.

Funder

European Union

Greek national funds

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference43 articles.

1. Unmanned Aircraft Systems: UAVS Design, Development and Deployment;Austin,2010

2. Conceptual design of a blended wing body MALE UAV;Panagiotou;Aerosp. Sci. Technol.,2018

3. Aerodynamic design of a MALE UAV;Panagiotou;Aerosp. Sci. Technol.,2016

4. Conceptual design of a UAV with VTOL characteristics;Kaparos,2019

5. Aerodynamic and aeroelastic uncertainty quantification of NATO STO AVT-251 unmanned combat aerial vehicle;Da Ronch;Aerosp. Sci. Technol.,2019

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