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1

Lucio, Maestrello, Bayliss Alvin, and Langley Research Center, eds. Coupling between plate vibration and acoustic radiation. National Aeronautics and Space Administration, Langley Research Center, 1992.

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2

P, Townsend Dennis, Coy John J, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Minimization of the vibration energy of thin-plate structure. National Aeronautics and Space Administration, 1992.

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3

E, Kielb Robert, ed. Joint research effort on vibrations of twisted plates: Phase 1, final results. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

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4

H, Williams James. Modes of vibration on square fiberglass epoxy composite thick plate. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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5

C, Marques Elizabeth R., Lee Samson S, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Massachusetts Institute of Technology, and Lewis Research Center, eds. Modes of vibration on square fiberglass epoxy composite thick plate. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

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6

Xiang, Y. Plate vibration with arbitrarily oriented stiffeners based on Mindlin-Engesser formulation. Department of Civil Engineering, University of Queensland, 1993.

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7

Y, Xiang, ed. Plate vibration with arbitrarily oriented stiffners based on Mindlin-Engesser formulation. University of Queensland, Dept. of Civil Engineering, 1993.

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8

L, Krantz T., and United States. National Aeronautics and Space Administration., eds. Minimization of the vibration energy of thin-plate structures and the application to the reduction of gearbox vibration. National Aeronautics and Space Administration, 1995.

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9

L, Krantz T., and United States. National Aeronautics and Space Administration., eds. Minimization of the vibration energy of thin-plate structures and the application to the reduction of gearbox vibration. National Aeronautics and Space Administration, 1995.

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10

M, Morales Adolfo, and Dryden Flight Research Facility, eds. The effects of excitation waveforms and shaker moving mass on the measured modal characteristics of a 2- by 5-foot aluminum plate. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1989.

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11

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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12

R, Emeric P., and Institute for Computer Applications in Science and Engineering., eds. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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13

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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14

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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15

Banks, H. Thomas. Detection of non-symmetrical damage in smart plate-like structures. Institute for Computer Applications in Science and Engineering, NASA Langley Research Center, 1998.

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16

Anderson, Melvin S. Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate asemblies. Langley Research Center, 1993.

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17

Yuan, Weixing. Buckling and vibration of compact laminated and sandwich plate structures by a refined spline finite strip analysis. University of Birmingham, 1999.

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18

Center, Langley Research, ed. Mobility power flow analysis of coupled plate structure subjected to mechanical and acoustic excitation. National Aeronautics and Space Administration, Langley Research Center, 1992.

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19

Mohd, Sabarudin bin. Vibration and buckling analysis of laminated plate and shell structures by thin and shear deformable curved finite strips. University of Birmingham, 1990.

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20

Liu, Meilan, and Cho W. S. To, eds. Vibration and Nonlinear Dynamics of Plates and Shells - Applications of Flat Triangular Finite Elements. BENTHAM SCIENCE PUBLISHERS, 2014. http://dx.doi.org/10.2174/97816080577191140101.

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21

Dorie, Carmine. Whole Body Vibration No Need Vibration Plate for Good Health: Human Body Vibration Book. Independently Published, 2020.

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22

National Aeronautics and Space Administration (NASA) Staff. Minimization of the Vibration Energy of Thin-Plate Structures and the Application to the Reduction of Gearbox Vibration. Independently Published, 2018.

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23

Interaction of acoustic waves generated by coupled plate. Center for Acoustics and Vibration, Florida Atlantic University, 1990.

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24

National Aeronautics and Space Administration (NASA) Staff. Static and Vibration Analyses of General Wing Structures Using Equivalent Plate Models. Independently Published, 2018.

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25

Wu, Zhonghui. Optimized Multi-Modes Mimo Positive Position Feedback Active Vibration for Plate Structure. GRIN Verlag GmbH, 2016.

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26

Simultaneous Composite Tailoring and Bending Control Optimization for Damping the Torsional Vibration of a Plate. Storming Media, 1996.

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27

Inclusion of transverse shear deformation in the exact buckling and vibration analysis of composite plate assemblies. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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28

National Aeronautics and Space Administration (NASA) Staff. Inclusion of Transverse Shear Deformation in the Exact Buckling and Vibration Analysis of Composite Plate Assemblies. Independently Published, 2018.

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29

Shahrjerdi, A. Second Order Shear Deformation Theory (SSDT) for Free Vibration Analysis on a Functionally Graded Quadrangle Plate. INTECH Open Access Publisher, 2011.

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30

Wu, Zhonghui. Active Vibration Control of Plate Structure Using Electromagnetic Transducer Based on H_ Optimized Positive Position Feedback. GRIN Verlag GmbH, 2016.

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31

Iutam Symposium On Relations Of Shell Plate Beam And 3d Models Proceedings Of The Iutam Symposium On The Relations Of Shell Plate Beam And 3d Models Dedicated To The Centenary Of Ilia Vekuas Birth Held In Tbilisi Georgia April 2327 2007. Springer, 2008.

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32

Mobility power flow analysis of coupled plate structure subjected to mechanical and acoustic excitation. National Aeronautics and Space Administration, Langley Research Center, 1992.

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33

Mobility power flow analysis of coupled plate structure subjected to mechanical and acoustic excitation: Final report. Florida Atlantic University, Dept. of Ocean Engineering, 1991.

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