Leading Edge Serrations on Flat Plates at Low Reynolds Number-Reference-Cited by-同舟云学术

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Leading Edge Serrations on Flat Plates at Low Reynolds Number

Published:2012-01-09 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
language:
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Author:

Cranston Brian¹,Laux Chris²,Altman Aaron¹

Affiliation:

1. University of Dayton

2. The University of Dayton

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2012-53

Reference26 articles.

1. [2]Torres. G.E. and Mueller, T.J. "Aerodynamic Characteristicsof Low Aspect Ratio Wingsat Low ReynoldsNumbers", Chapter 7, pp.115-140, Fixedand Flapping Wing Aerodynamics forMicro Air Vehicle Applications, AIAAProgressin Aeronauticsand Astronautics, Vol.195,2001.

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1. Compressibility effects on flat-plates with serrated leading-edges at a low Reynolds number;Experiments in Fluids;2017-10-23

2. An experimental study of an airfoil with a bio-inspired leading edge device at high angles of attack;Smart Materials and Structures;2017-08-17

3. Features of owl wings that promote silent flight;Interface Focus;2017-02-06

4. Mimicking the humpback whale: An aerodynamic perspective;Progress in Aerospace Sciences;2016-07

5. Streamwise counter-rotating vortices generated by triangular leading edge pattern in flat plate boundary layer;Journal of Visualization;2016-01-05

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