Natural frequencies and modal shapes of folded sandwich plates made of porous core and FG-CNTRC coating layers resting on two parameters elastic foundation
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Published:2024-05
Issue:
Volume:148
Page:109077
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ISSN:1270-9638
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Container-title:Aerospace Science and Technology
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language:en
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Short-container-title:Aerospace Science and Technology
Author:
Salehipour Hamzeh,
Shahmohammadi Mohammad Amin,
Civalek ÖmerORCID
Reference41 articles.
1. Calculation of hinge moments for a folding wing aircraft based on high-order panel method;Xu;Math. Prob. Eng.,2020
2. Structural dynamics model of multisegmented folding wings: theory and experiment;Wang;J. Aircraft,2011
3. Lockheed F-117 Nighthawk Stealth Fighter;Crickmore,2014
4. J. Gibb, B. Scott, A case study: integrating triple-junction solar cells into flat-folding flexible solar array panels, in: 35th IEEE Photovoltaic Specialists Conference, 2010.
5. D.H. Lee, T.A. Weishaar, Aeroelastic studies on a folding wing configuration, in: 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, 2005.
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