New Actuation Methods for Miniature Trailing-Edge Effectors for Rotorcraft-Reference-Cited by-同舟云学术

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New Actuation Methods for Miniature Trailing-Edge Effectors for Rotorcraft

Published:2009-05-04 Issue: Volume: Page:
ISSN:
Container-title:50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Thiel Michael¹,Lesieutre George¹

Affiliation:

1. Pennsylvania State University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2009-2104

Reference11 articles.

1. Design of Subsonic Airfoils for High Lift

2. Miniature Trailing-Edge Effectors for Rotorcraft Performance Enhancement

3. 3Kinzel, M.P. "Miniature Trailing-Edge Effectors for Rotorcraft Applications," M.S. Thesis, Department of Aerospace Engineering, ThePennsylvania State University, August 2004.

4. 4Lieshman,L.G.,PrinciplesofHelicopterAerodynamics,CambridgeUniversityPress,NewYork,NY,2001.

Cited by 1 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. Geometrical optimization of a hingeless deployment system for an active rotor blade;Journal of Intelligent Material Systems and Structures;2012-10-09

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