A Computational Study of Induced Drag Behavior for Spanwise Cambered Wings-Reference-Cited by-同舟云学术

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A Computational Study of Induced Drag Behavior for Spanwise Cambered Wings

Published:2010-06-28 Issue: Volume: Page:
ISSN:
Container-title:28th AIAA Applied Aerodynamics Conference
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Author:

Pomeroy Brent¹,Visser Kenneth¹

Affiliation:

1. Clarkson University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2010-4227

Reference33 articles.

1. 1Munk,Maxwell."TheMinimumInducedDragofAirfoils." NACATR121,1921.

2. 2Brandt,Steven A.IntroductiontoAeronautics:ADesignPerspective.Ed.JosephA.Schetz.2nded.Reston,VA:AmericanInstitute ofAeronauticsandAstronautics,2004.

3. 4Pomeroy,Walter.Privatephoto.Usedbypermission.2006.

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. Aerodynamic Shape Optimization of Highly Nonplanar Raised and Drooped Wings;Journal of Aircraft;2022-01

2. Optimal Hyperelliptic Cambered Span Configurations for Minimum Drag;Journal of Aircraft;2019-01

3. Wing-Body and Vertical Tail Interference Effects on Downwash Rate of the Horizontal Tail in Subsonic Flow;Journal of Aerospace Engineering;2017-07

4. Towards an Effective Nonplanar Wing Design Strategy;34th AIAA Applied Aerodynamics Conference;2016-06-10

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