Computational Fluid Dynamic Study on a Novel Propulsive System: ACHEON and Its Integration with an Unmanned Aerial Vehicle (UAV)-Reference-Cited by-同舟云学术

Computational Fluid Dynamic Study on a Novel Propulsive System: ACHEON and Its Integration with an Unmanned Aerial Vehicle (UAV)

Published:2016-01 Issue:1 Volume:29 Page:04015015
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Das Shyam S.¹,Páscoa Jose C.²,Trancossi M.³,Dumas A.³

Affiliation:

1. Post Doctoral Researcher, Dept. of Electromechanical Engineering, Center for Mechanical and Aerospace Sciences and Technology (C-MAST), Univ. of Beira Interior, R. Mq.s D’Ávila e Bolama, 6201-001 Covilhã, Portugal (corresponding author).

2. Professor, Dept. of Electromechanical Engineering, Univ. of Beira Interior, 6201-001 Covilhã, Portugal.

3. Professor, DISMI—Dipartimento di Scienze e Metodi dell’Ingegneria, Università degli Studi di Modena e Reggio Emilia, Via Amendola 2, Pad. Morselli, 42122 Reggio Emilia, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000498

Reference39 articles.

1. Modified split-potential model for modeling the effect of DBD plasma actuators in high altitude flow control

2. ACHEON. (2011). “Acheon project.” 〈http://acheon.eu/project/〉 (Jan. 12 2012).

3. ACHEON. (2014). “V/STOL handling i-criteria and discussion.” Technical Rep. AGARD-R-577-70 Advisory Group for Aerospace Research and Development.

4. Aerodynamic Design and Characterization of a Quad Tilt-Wing UAV via Wind Tunnel Tests

5. Clarke A. J. (2011). “The conceptual design of novel future UAV’s incorporating advanced technology and research components.” Ph.D. thesis School of Engineering Cranfield Univ. U.K.

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