Dynamic response analysis of the helicopter blades with non-uniform structural properties
Author:
Affiliation:
1. Carleton University
2. Kopter Germany GmbH
Publisher
American Institute of Aeronautics and Astronautics
Reference18 articles.
1. Geometrically Exact, Intrinsic Theory for Dynamics of Curved and Twisted Anisotropic Beams
2. On the energy of an elastic rod
3. Hodges, D.H., 1990. "A mixed variational formulation based on exact intrinsic equations for dynamics of moving beams," International Journal of Solids and Structures 26, 1253-1273.
4. VABS: A New Concept for Composite Rotor Blade Cross-Sectional Modeling
5. Variational asymptotic beam sectional analysis – An updated version
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1. Dynamic Modeling and Analysis of Helicopter Transmission System Considering the Effect of Input Conditions;Mechanisms and Machine Science;2024
2. A semianalytical approach for the variational asymptotic sectional analysis of a beam with high values of initial twist and curvatures;Journal of Mechanics of Materials and Structures;2023-04-18
3. A harmonic balance solution for the intrinsic 1D nonlinear equations of the beams;Journal of Vibration and Control;2023-03-13
4. Modal analysis of twisted and curved blades using geometrically exact, intrinsic equations and general boundary conditions;AIAA SCITECH 2023 Forum;2023-01-19
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