2023
DOI: 10.2514/1.c036894
|View full text |Cite
|
Sign up to set email alerts
|

Finite Element Model Updating for Very Flexible Wings

Abstract: As aircraft wings become more flexible as a result of searching for more fuel efficient and higher performance solutions, structural nonlinearities become more apparent. Geometric nonlinearities make the structure’s modal parameters a function of the deformed shape and therefore of the loading condition. Modal characterization of very flexible structures is challenging due to these nonlinearities and the very low natural frequencies (the fundamental mode is typically below 1 Hz). In traditional, stiffer struct… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
1

Citation Types

0
1
0

Year Published

2024
2024
2024
2024

Publication Types

Select...
2
1

Relationship

0
3

Authors

Journals

citations
Cited by 3 publications
(1 citation statement)
references
References 27 publications
0
1
0
Order By: Relevance
“…However, discrepancies between computed outcomes and experimental measurements can limit the model's suitability for precise assessments of structural behavior. Various strategies for model calibration have been developed across different fields, such as those proposed in [26] for composite fuselages and those discussed in [27] for wings.…”
Section: Model Updating Techniquesmentioning
confidence: 99%
“…However, discrepancies between computed outcomes and experimental measurements can limit the model's suitability for precise assessments of structural behavior. Various strategies for model calibration have been developed across different fields, such as those proposed in [26] for composite fuselages and those discussed in [27] for wings.…”
Section: Model Updating Techniquesmentioning
confidence: 99%