Fundamental investigation into output-based prediction of whirl flutter bifurcations-Reference-Cited by-同舟云学术

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Fundamental investigation into output-based prediction of whirl flutter bifurcations

Published:2023-11 Issue: Volume:123 Page:103986
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Gali Sai Vishal,Goehmann Todd G.,Riso Cristina^ORCID

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference73 articles.

1. Investigation of propeller-power-plant autoprecession boundaries for a dynamic-aeroelastic model of a four-engine turboprop transport airplane;Abbott Jr.,1963

2. High speed whirl flutter tests of the maryland tiltrotor rig;Akinwale,2023

3. Numerical Continuation Methods: An Introduction;Allgower,2012

4. Braniff airways flight 542 accident;Anon,1961

5. Northwest airlines flight 710 accident;Anon,1961

Cited by 3 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. Limit-Cycle Oscillation Prediction in Supersonic Panels Using Pre-Flutter Transient Responses;AIAA SCITECH 2024 Forum;2024-01-04

2. A Sliding-Window Matrix Pencil Method for Aeroelastic Design Optimization with Limit-Cycle Oscillation Constraints;AIAA SCITECH 2024 Forum;2024-01-04

3. Output-Based Prediction of Whirl Flutter Limit-Cycle Oscillations Considering Multiple Varying Parameters;AIAA SCITECH 2024 Forum;2024-01-04

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