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Topology Optimization for Vibration and Noise Reduction of Stiffened Thin Plate Structures
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Lei Hu1, Yuqi Sun1, Jintao Zhang2, Jialiang Sun2, Minqiang Shao2,
Journal of Dynamics and Control | 2025, 23(10) : 61 - 67
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Journal of Dynamics and Control | 2025, 23(10): 61-67
Research Articles
Topology Optimization for Vibration and Noise Reduction of Stiffened Thin Plate Structures
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Lei Hu1, Yuqi Sun1, Jintao Zhang2, Jialiang Sun2, Minqiang Shao2,
Affiliations
  • 1. Shenyang Aircraft Design and Research Institute, Shenyang 110035, China
  • 2. State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
doi: 10.6052/1672-6553-2025-053
Outline
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Low- and medium-frequency noise induces vibrations to the cabin structure, which subsequently radiates noise into the interior. In order to solve the vibration and noise optimization problem of stiffened thin plates, this study employs topology optimization to enhance the vibration and noise reduction effects by optimizing the layout of stiffeners. This study focuses on four-edge clamped stiffened thin plates and employs density-based topology optimization method to maximize its first-order modal frequency. Under the constraint of constant mass, the optimal distribution of stiffeners on the plate is designed. Modal, stiffness, and sound transmission loss analyses are conducted for the stiffened thin plate before and after optimization. The results show that the optimized stiffened plate achieves an increase in its first-order modal frequency and improves sound transmission loss within a certain frequency range, without significantly reducing the overall stiffness.

stiffened thin plate  /  topology optimization  /  modal frequency  /  sound transmission loss
Lei Hu, Yuqi Sun, Jintao Zhang, Jialiang Sun, Minqiang Shao. Topology Optimization for Vibration and Noise Reduction of Stiffened Thin Plate Structures[J]. Journal of Dynamics and Control, 2025 , 23 (10) : 61 -67 . DOI: 10.6052/1672-6553-2025-053
  • National Natural Science Foundation of China(12372042)
Year 2025 volume 23 Issue 10
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Article Info
doi: 10.6052/1672-6553-2025-053
  • Receive Date:2024-12-28
  • Online Date:2026-03-20
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History
  • Received:2024-12-28
  • Revised:2025-04-15
Funding
National Natural Science Foundation of China(12372042)
Affiliations
    1. Shenyang Aircraft Design and Research Institute, Shenyang 110035, China
    2. State Key Laboratory of Mechanics and Control for Aerospace Structures, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
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表12种不同金属材料的力学参数

Family
属数
Number of
genus
种数
Number of
species
占总种数比例
Percentage of
total species (%)

Genus
种数
Number of
species
占总种数比例
Percentage of total
species (%)
鹅膏菌科Amanitaceae 2 11 5.26 鹅膏菌属 Amanita 10 4.78
小菇科 Mycenaceae 2 12 5.74 丝盖伞属 Inocybe 5 2.39
多孔菌科 Polyporaceae 8 14 6.70 蜡蘑属 Laccaria 5 2.39
红菇科 Russulaceae 3 23 11.00 小皮伞属 Marasmius 6 2.87
小菇属 Mycena 11 5.26
光柄菇属 Pluteus 5 2.39
红菇属 Russula 17 8.13
栓菌属 Trametes 5 2.39
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