Rotorcraft fuselage/main rotor coupling dynamics modelling and analysis

DOI10.1515/ijnsns-2019-0102OpenAlexW3094824781MaRDI QIDQ2235335

Salvador Castillo-Rivera, Maria Tomás-Rodríguez

Publication date: 21 October 2021

Published in: International Journal of Nonlinear Sciences and Numerical Simulation (Search for Journal in Brave)

Full work available at URL: https://openaccess.city.ac.uk/id/eprint/24971/1/MTR%20Salvador.pdf

zbMATH Keywords

rotormodal analysisfuselageheterodyning

Mathematics Subject Classification ID

Mechanics of particles and systems (70-XX) Systems theory; control (93-XX)

Related Items (1)

VehicleSim

Cites Work

• Unnamed Item
• System identification methods for (operational) modal analysis: review and comparison
• The modal analysis of a motorcycle in straight running and on a curve
• Nonlinear autopilot control design for a 2-DOF helicopter model
• Identification of linear parameter-varying state-space models with application to helicopter rotor dynamics
• Principles of Astrophysical Fluid Dynamics
• Coupled rotor/fuselage vibration analysis using detailed 3-D airframe models.
• Modeling rotorcraft dynamics with finite element multibody procedures.

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