Dynamic Fluid-Structure Coupling Method of Flexible Flapping Wing for MAV-Reference-Cited by-同舟云学术

Dynamic Fluid-Structure Coupling Method of Flexible Flapping Wing for MAV

Author:

Yang Wenqing¹,Song Bifeng²,Wang Liguang³,Chen Lili⁴

Affiliation:

1. Assistant Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China (corresponding author).

2. Professor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

3. Postdoctor, School of Aeronautics, Northwestern Polytechnical Univ., Xi’an 710072, China.

4. Aviation Industry Corporation of China, First Aircraft Institute, No. 1 East Renmin Rd., Yanliang, Xi’an 710089, China.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

Reference33 articles.

4. A rational engineering analysis of the efficiency of flapping flight;Hall K. C.;Prog. Astronaut. Aeronaut.,2001

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