Investigation on Excitation Equivalence Technique for Thin-Walled Panel Based on Pseudo-excitation Method-Reference-Cited by-同舟云学术

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Investigation on Excitation Equivalence Technique for Thin-Walled Panel Based on Pseudo-excitation Method

Published:2022-08-18 Issue:4 Volume:23 Page:702-710
ISSN:2093-274X
Container-title:International Journal of Aeronautical and Space Sciences
language:en
Short-container-title:Int. J. Aeronaut. Space Sci.

Author:

Zhou Hong-wei^ORCID,Yan Qun,Guo Ding-wen,Wang Yan

Funder

Advance Research of Equipment of China

Aeronautical Science Foundation of China

Publisher

Springer Science and Business Media LLC

Subject

Electrical and Electronic Engineering,Aerospace Engineering,General Materials Science,Control and Systems Engineering

Link

https://link.springer.com/content/pdf/10.1007/s42405-022-00487-y.pdf

Reference12 articles.

1. Morton M, Hampson, C, Alexander R (2008) Final vibration and acoustic loads development for certification of the F-22 Advanced tactical fighter. In: 49th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference, 16th AIAA/ASME/AHS Adaptive Structures Conference,10th AIAA Non-Deterministic Approaches Conference, 9th AIAA Gossamer Spacecraft Forum, 4th AIAA Multidisciplinary Design Optimization Specialists Conference. https://doi.org/10.2514/6.2008-1901

2. Liguore S, Thomas M, Pitt D (2012) Application and demonstration of nonlinear reduced order modeling (NLROM) for thermal/acoustic response. In: 53rd AIAA/ASME/ASCE/AHS/ASC structures, structural dynamics and materials conference, pp 1–12. https://doi.org/10.2514/6.2012-1626

3. Joo Y-S, Lee J-C (2021) Vibration fatigue analysis for structural durability evaluation under vibratory loads. Int J Aeronaut Space Sci 22:578–589. https://doi.org/10.1007/s42405-020-00326-y

4. Yan TF, Zhang JG, Fang GQ, Shen ZQ (2014) A comparison between vibro-acoustic environment test and single environment test for a spacecraft antenna. Spacecr Environ Eng 31(2):154–157. https://doi.org/10.12126/see.2014.02.008 (in Chinese)

5. Leung K, Foist B (1995) Prediction of acoustically induced random vibration loads for shuttle payloads. In: 36th Structures, Structural Dynamics and Materials Conference. https://doi.org/10.2514/6.1995-1200

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