When an airplane undergoes symmetric vibrations, Fig.

Vortex-Induced Vibrations of Flexible Beams

SOLVED: The vibration in the vertical direction of an airplane and its wings can be modeled as a 3-DOF system, with stiffness connecting the three masses corresponding to that of the wing

Free vibration and buckling response of functionally graded triply periodic minimal surface beams considering neutral axis dislocation - Mithilesh Kurup, Jeyaraj Pitchaimani, 2023

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

An asymmetric bistable vibro-impact DEG for enhanced ultra-low-frequency vibration energy harvesting - ScienceDirect

Aerospace, Free Full-Text

PDF) Calibration of a Nose Boom Mounted Airflow Sensor on an Atmospheric Research Aircraft by Inflight Maneuvers

Free vibration and buckling response of functionally graded triply periodic minimal surface beams considering neutral axis dislocation - Mithilesh Kurup, Jeyaraj Pitchaimani, 2023

Direct numerical simulation of a counter-rotating vortex pair interacting with a wall, Journal of Fluid Mechanics