Low Reynolds Number Behavior of a Solid-State Piezocomposite Variable-Camber Wing-Reference-Cited by-同舟云学术

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Low Reynolds Number Behavior of a Solid-State Piezocomposite Variable-Camber Wing

Published:2013-04-05 Issue: Volume: Page:
ISSN:
Container-title:54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference
language:
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Author:

Bilgen Onur¹,Friswell Michael²,Landman Drew¹

Affiliation:

1. Old Dominion University

2. Swansea University

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2013-1515

Reference39 articles.

1. A Review of Morphing Aircraft

2. Eggleston,G.,Hutchison,C.,Johnston,C.,Koch,B.,Wargo,G.andWilliams,K."MorphingAircraftDesignTeam,"Virginia TechAerospaceEngineeringSenior Design Project, 2002.

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