Experimental and Computational Investigation of Blunt Trailing-Edge Airfoils with Splitter Plates-Reference-Cited by-同舟云学术

Experimental and Computational Investigation of Blunt Trailing-Edge Airfoils with Splitter Plates

Published:2018-08 Issue:8 Volume:56 Page:3229-3239
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Metzinger Camille N.¹,Chow Raymond¹,Baker Jonathon P.¹,Cooperman Aubryn M.¹,van Dam C. P.¹

Affiliation:

1. University of California, Davis, Davis, California 95616

Funder

Sandia National Laboratories

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

https://arc.aiaa.org/doi/am-pdf/10.2514/1.J056098

Reference34 articles.

1. JacksonK. J.ZuteckM. D.van DamC. P.StandishK. J.BerryD. “Innovative Design Approaches for Large Wind Turbine Blades,” Wind Energy, Vol. 8, April 2005, pp. 141–171. doi:10.1002/we.128

2. Innovative design approaches for large wind turbine blades

3. Computational investigations of blunt trailing-edge and twist modifications to the inboard region of the NREL 5 MW rotor

4. Aerodynamic Analysis of Blunt Trailing Edge Airfoils

5. BakerJ. P.van DamC. P.GilbertB. L. “Flatback Airfoil Wind Tunnel Experiment,” Rept. SAND2008-2008, Sandia National Lab., Albuquerque, NM, April 2008.

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