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Helicopter Rotor Load Prediction Using a Geometrically Exact Beam with Multicomponent Model

机译：用多组分模型的几何精确梁预测直升机转子载荷

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Hyun-ku Lee; S. R. Viswamurthy; Sang Chul Park; Taeseong Kim; Sang Joon Shin; Deog-kwan Kim;
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年度 2010
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1. Helicopter Rotor Load Prediction Using a Geometrically Exact Beam with Multicomponent Model [J] . Hyun-Ku Lee, S. R. Viswamurthy, Sang Chul Park, Journal of Aircraft . 2010,第4期

机译：基于几何精确梁的多组件模型的直升机旋翼载荷预测
2. Helicopter Rotor Load Prediction Using a Geometrically Exact Beam with Multicomponent Model [J] . Hyun-Ku Lee, S. R. Viswamurthy, Sang Chul Park, Journal of Aircraft . 2010,第4期

机译：基于几何精确梁的多组件模型的直升机旋翼载荷预测
3. Prediction of Helicopter Rotor Loads Using Time-Spectral Computational Fluid Dynamics and an Exact Fluid-Structure Interface [J] . Seongim Choi, Anubhav Datta, Juan J. Alonso Journal of the American Helicopter Society . 2011,第4期

机译：使用时谱计算流体动力学和精确的流体结构界面预测直升机旋翼载荷
4. Helicopter Rotor Load Prediction Using a Geometrically Exact Beam Theory with Multibody Dynamics [C] . S R Viswamurthy, Sang Chul Park, SangJoon Shin 34th European rotorcraft forum: post-conference CD . 2008

机译：基于多体动力学的几何精确梁理论的直升机旋翼载荷预测
5. Reduced Order Model-Based Prediction of the Nonlinear Geometric Response of a Panel Under Thermal, Aerodynamic, and Acoustic Loads. [D] . Matney, Andrew. 2014

机译：基于降阶模型的面板在热，空气动力和声载荷下的非线性几何响应预测。
6. On the geometrically exact low-order modelling of a flexible beam: formulation and numerical tests [O] . C. Howcroft, R. G. Cook, S. A. Neild, -1

机译：关于柔性梁的几何精确低阶建模：公式和数值测试
7. Helicopter Rotor Load Prediction Using a Geometrically Exact Beam with Multicomponent Model [O] . Lee Hyun-Ku, Viswamurthy S.R., Park Sang Chul, 2010

机译：用多组分模型的几何精确梁预测直升机转子载荷
8. Limits on the prediction of helicopter rotor noise using thickness and loading sources: Validation of helicopter noise prediction techniques [R] . Succi, G. P. 1983

机译：使用厚度和载荷源预测直升机旋翼噪声的限制：直升机噪声预测技术的验证

Helicopter Rotor Load Prediction Using a Geometrically Exact Beam with Multicomponent Model

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