Short Landing Performance and Scale Effect of a Flapping Wing Aircraft-Reference-Cited by-同舟云学术

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Short Landing Performance and Scale Effect of a Flapping Wing Aircraft

Published:2020-11 Issue:6 Volume:33 Page:04020085
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Chen Si¹^ORCID,Guo Shijun²,Li Hao³,Tong Mingbo⁴,Ji Bing⁵

Affiliation:

1. Ph.D. Student, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, PR China. ORCID: .

2. Professor, School of Aerospace, Transport and Manufacturing, Cranfield Univ., Cranfield MK43 0AL, UK (corresponding author).

3. Ph.D. Student, School of Aerospace, Transport and Manufacturing, Cranfield Univ., Cranfield MK43 0AL, UK.

4. Professor, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, PR China.

5. Associate Professor, School of Control Science and Engineering, Shandong Univ., Jinan 250061, PR China.

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.1943-5525.0001198

Reference29 articles.

1. Akturk A. A. Shavalikul and C. Camci. 2009. “PIV measurements and computational study of a 5-inch ducted fan for V/STOL UAV applications.” In Proc. 47th AIAA Aerospace Sciences Meeting. Reston VA: American Institute of Aeronautics and Astronautics.

2. Non-linear unsteady aerodynamic model for insect-like flapping wings in the hover. Part 2: Implementation and validation

3. Bio-inspired bi-plane flapping wing MAV;Baligidad S. M.;Open J. Mech. Eng. (OJME),2017

4. Kinematics and power requirements of ascending and descending flight in the pigeon (Columba livia)

5. Unsteady aerodynamic model of flexible flapping wing

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