Advanced Dynamic Vibration of Terfenol-D Control Law on Functionally Graded Material Plates/Cylindrical Shells in Unsteady Supersonic Flow

The thermal vibration of thick Terfenol-D control law on functionally graded material (FGM) plates/cylindrical shells in nonlinear unsteady supersonic flow with third-order shear deformation theory (TSDT) is investigated by using the generalized differential quadrature (GDQ) method. The effects of the coefficient term of TSDT displacement models on the thermal stress and center displacement of Terfenol-D control law on FGM plates/cylindrical shells in nonlinear unsteady supersonic flow are investigated. The coefficient term of TSDT models of thick Terfenol-D control law on FGM plates/cylindrical shells provide an additional effect on the values of displacements and stresses.

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Publication Details

Journal
Algorithms
Published
2025-02-06
DOI
https://doi.org/10.3390/a18020091
Citations
1
Primary Topic
Composite Structure Analysis and Optimization
Type
article
Field-Weighted Citation Impact
0.86
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article

Advanced Dynamic Vibration of Terfenol-D Control Law on Functionally Graded Material Plates/Cylindrical Shells in Unsteady Supersonic Flow

C.C. Hong
1 citations
Algorithms
Composite Structure Analysis and Optimization
0.86
article

Advanced Dynamic Vibration of Terfenol-D Control Law on Functionally Graded Material Plates/Cylindrical Shells in Unsteady Supersonic Flow

C.C. Hong
article en
1 citations

Abstract

The thermal vibration of thick Terfenol-D control law on functionally graded material (FGM) plates/cylindrical shells in nonlinear unsteady supersonic flow with third-order shear deformation theory (TSDT) is investigated by using the generalized differential quadrature (GDQ) method. The effects of the coefficient term of TSDT displacement models on the thermal stress and center displacement of Terfenol-D control law on FGM plates/cylindrical shells in nonlinear unsteady supersonic flow are investigated. The coefficient term of TSDT models of thick Terfenol-D control law on FGM plates/cylindrical shells provide an additional effect on the values of displacements and stresses.

AlgorithmsVol. 18(2)
Hsiuping University of Science and Technology (TW)
Openalex Percentile: Top 35%
Composite Structure Analysis and Optimization
0.86
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