Comparison of in-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches-Reference-Cited by-同舟云学术

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Comparison of in-Flight Measured and Computed Aeroelastic Damping: Modal Identification Procedures and Modeling Approaches

Published:2016-05-31 Issue:2 Volume:8 Page:163-177
ISSN:2175-9146
Container-title:Journal of Aerospace Technology and Management
language:
Short-container-title:J.Aerosp. Technol. Manag.

Author:

Follador Roberto Da Cunha,Souza Carlos Eduardo de,Marto Adolfo Gomes,Silva Roberto Gil Annes da,Góes Luis Carlos Sandoval

Publisher

FapUNIFESP (SciELO)

Subject

Aerospace Engineering

Cited by 13 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. A data-driven approach for rapid detection of aeroelastic modes from flutter flight test based on limited sensor measurements;Mechanical Systems and Signal Processing;2024-11

2. A Dynamic Mode Decomposition Based Approach for Rapid Detection of Aeroelastic Modes from Flutter Flight Test Data;AIAA AVIATION 2023 Forum;2023-06-08

3. In-flight modal identification by operational modal analysis;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2023-04-28

4. Normal Modes Study on Half Wing Structure of N219 Aircraft Using Computational Method;Advances in Science and Technology;2023-03-01

5. Pretest Planning Approach for Optimal Modal Testing on High Aspect Ratio Wing Structure;Iranian Journal of Science and Technology, Transactions of Mechanical Engineering;2022-12-03

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