Evaluation of Lift Formulas Applied to Low-Reynolds-Number Unsteady Flows-Reference-Cited by-同舟云学术

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Evaluation of Lift Formulas Applied to Low-Reynolds-Number Unsteady Flows

Published:2015-01 Issue:1 Volume:53 Page:161-175
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Wang Shizhao¹,Zhang Xing¹,He Guowei¹,Liu Tianshu²

Affiliation:

1. State Key Laboratory of Nonlinear Mechanics, Institute of Mechanics, Chinese Academy of Sciences, 100190 Beijing, People’s Republic of China

2. Department of Mechanical and Aerospace Engineering, Western Michigan University, Kalamazoo, Michigan 49008

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.J053042

Reference32 articles.

1. Flapping Wing Aerodynamics: Progress and Challenges

2. Flapping-Wing Aerodynamics

3. Micro air vehicle-motivated computational biomechanics in bio-flights: aerodynamics, flight dynamics and maneuvering stability

4. Hovering of model insects: simulation by coupling equations of motion with Navier–Stokes equations

5. A family of vortex wakes generated by a thrush nightingale in free flight in a wind tunnel over its entire natural range of flight speeds

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2. Aerodynamic Force and Vortex Force on Flapping Wings;AIAA AVIATION 2023 Forum;2023-06-08

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4. A frequency-domain formulation for predicting multi-frequency noise generated by flows with periodically moving boundaries;Journal of Theoretical and Computational Acoustics;2023-01-19

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