Dynamic Stability of a Rotor Blade Using Finite Element Analysis (Q3950069)
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| Language | Label | Description | Also known as |
|---|---|---|---|
| English | Dynamic Stability of a Rotor Blade Using Finite Element Analysis |
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Dynamic Stability of a Rotor Blade Using Finite Element Analysis (English)
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1982
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aeroelastic stability
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flap bending
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lead-lag bending
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torsion of helicopter rotor blade
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Hamilton's principle
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quasisteady two-dimensional airfoil theory
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aerodynamic loads
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discretized into beam elements
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ten nodal degrees of freedom
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nonlinear equations of motion
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steady-state blade deflections
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iterative procedure
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blade motion a small perturbation about steady solution
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normal mode method
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