Experimental Study of Impulsively Rotated Flat Plate at Low Reynolds Number-Reference-Cited by-同舟云学术

Experimental Study of Impulsively Rotated Flat Plate at Low Reynolds Number

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:40th Fluid Dynamics Conference and Exhibit
language:
Short-container-title:

Author:

Baik Yeon Sik¹,Aono Hikaru¹,Rausch Jonathan¹,Bernal Luis¹,Shyy Wei¹,Ol Michael²

Affiliation:

1. University of Michigan

2. U.S. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4462

Reference28 articles.

1. [1]Shyy, W.,Lian,Y.,Tang,J.,Viieru,D.&Liu,H.(2008).Aerodynamics of LowReynolds Number Flyers.Cambridge UniversityPress.

2. [3]Dickinson,M.H.&Gotz,K.G.(1993).Unsteadyaerodynamic performanceonmodel wings atlow Reynolds numbers.J.Exp.Biol ,Vol.174, pp.45-64.

3. The aerodynamics of hovering insect flight. IV. Aerodynamic mechanisms

4. [5]Maxworthy,T.(1979).ExperimentsontheWeis-Fogh mechanismof lift eneration byinsects in hoveringflight Part 1.Dynamics of the 'fling'.J.FluidMech.,Vol.93,pp.47-63.

Cited by 8 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. Feedback Flow Control: A Heuristic Approach;AIAA Journal;2018-10

2. A scaling for vortex formation on swept and unswept pitching wings;Journal of Fluid Mechanics;2017-10-26

3. Three-Dimensionality Effects due to Change in the Aspect Ratio for the Flow around an Impulsively Pitching Flat Plate;Journal of Aerospace Engineering;2017-09

4. Effects of Planform Geometry and Pivot Axis Location on the Aerodynamics of Pitching Low Aspect Ratio Wings;43rd Fluid Dynamics Conference;2013-06-22

5. Generating LEVs on Energetically Optimal, Flapping Wing Designs by Modulating Leading Edge Angle;31st AIAA Applied Aerodynamics Conference;2013-06-22