International Journal of Transportation Engineering and Technology
Volume 2, Issue 4-1, December 2016, Pages: 1-6
Received: Apr. 13, 2016;
Accepted: Jul. 22, 2016;
Published: Sep. 3, 2016
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Ngo Khanh Hieu, Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam
Pham Quang Vinh, Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam
Dinh Anh Bao, Department of Aerospace Engineering, Ho Chi Minh City University of Technology, Ho Chi Minh City, Vietnam
The design process of a product is a multi-step process of selection and assessment criteria to create a final product which meets all the needs of the practice. A small UAV combined between flying-wing and quadrotor is a very complex product, so the design process of this small UAV requires a thorough and circumspect review. The problem is how to optimize the design and to carry out the testing of the feasibility of design requirements with the lowest cost and time savings. For that reason, many tools of Multi-Fidelity Analysis for UAV such as XFLR5, XFoil… have been used to give considerable support for this design process. This research focusses mainly on the analysis/design of the configuration of a small UAV flying wing based on the performance at its cruise speed.
Ngo Khanh Hieu,
Pham Quang Vinh,
Dinh Anh Bao,
Design of a Small UAV Combined Between Flying-Wing and Quadrotor with XFRL5, International Journal of Transportation Engineering and Technology. Special Issue: Experiments Researches in Aeronautical Engineering.
Vol. 2, No. 4-1,
2016, pp. 1-6.
Copyright © 2016 Authors retain the copyright of this article.
This article is an open access article distributed under the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0/
) which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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