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Flutter control and mitigation of limit cycle oscillations in aircraft wings using distributed vibration absorbers.

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Bibliographic Details
Title: Flutter control and mitigation of limit cycle oscillations in aircraft wings using distributed vibration absorbers.
Authors: Basta, Ehab1, Ghommem, Mehdi1, mghommem@aus.edu, Emam, Samir1
Source: Nonlinear Dynamics; Nov2021, Vol. 106 Issue 3, p1975-2003, 29p
Database: Applied Science & Technology Source
Description
ISSN:0924090X
DOI:10.1007/s11071-021-06889-z