Experimental Results from the Active Aeroelastic Wing Wind Tunnel Test Program-Reference-Cited by-同舟云学术

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Experimental Results from the Active Aeroelastic Wing Wind Tunnel Test Program

Published:2005-04-18 Issue: Volume: Page:
ISSN:
Container-title:46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
language:
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Author:

Heeg Jennifer¹,Spain Vic¹,Florance James¹,Wieseman Carol¹,Ivanco Tom¹,DeMoss Josh¹,Silva Walt¹,Panetta Andrew²,Lively Peter³,Tumwa Vic⁴

Affiliation:

1. NASA Langley Research Center

2. SWALES Aerospace

3. Lockheed Martin Space Operations

4. Jacobs-Sverdrup

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2005-2234

Reference15 articles.

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. Distributed Sensing of a Cantilever Beam and Plate using a Fiber Optic Sensing System;2018 Applied Aerodynamics Conference;2018-06-24

2. Aircraft Active Flutter Suppression: State of the Art and Technology Maturation Needs;Journal of Aircraft;2018-01

3. A Composite Wing Structure with a Morphing Leading Edge;51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 18th AIAA/ASME/AHS Adaptive Structures Conference<BR> 12th;2010-04-12

4. Static Aeroelastic and Open-Loop Aeroservoelastic Analyses for the F/A-18 AAW Aircraft;48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference;2007-04-23

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