Numerical Study of Two Flapping Airfoils in Tandem Configuration-Reference-Cited by-同舟云学术

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Numerical Study of Two Flapping Airfoils in Tandem Configuration

Published:2010-01-04 Issue: Volume: Page:
ISSN:
Container-title:48th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition
language:
Short-container-title:

Author:

Broering Timothy¹,Lian Yongsheng¹,Henshaw William²

Affiliation:

1. University of Louisville

2. Lawrence Livemore National Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-865

Reference25 articles.

1. Grasmeyer, J.M. and Keennon, M.T. "Development of the Black Widow Micro Air Vehicle," AIAA PaperNo.2001-0127,2001.

2. Pornsin-Sirirak, T.N., Tai, Y-C., Ho, C-M., and Keennon, M. "Microbat: A Palm-Sized Electrically Powered Ornithoper,"http://ho.seas.ucla.edu/publications/conference/2001/jpl10_2001.pdf.

3. Low-Reynolds-Number Airfoils

Cited by 4 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Force and Flow Field Measurement System for Tandem Flapping Wings;Experimental Techniques;2016-07-18

2. Experimental study on instantaneous thrust and lift of two plunging wings in tandem;Experiments in Fluids;2015-12-24

3. Experimental Study on Mean Thrust of Two Plunging Wings in Tandem;AIAA Journal;2015-06

4. Recent progress in flapping wing aerodynamics and aeroelasticity;Progress in Aerospace Sciences;2010-10

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