首页> 外文会议>AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference >The AVINOR Aeroelastic Simulation Code and Its Application to Reduced Vibration Composite Rotor Blade Design

【24h】

The AVINOR Aeroelastic Simulation Code and Its Application to Reduced Vibration Composite Rotor Blade Design

机译：AVINOR气弹仿真代码及其在减振复合材料转子叶片设计中的应用

获取原文

页面导航

著录项
相似文献
相关主题

著录项

来源
《AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference》|2009年|P.1-34|共34页
会议地点
作者
B. Glaz; P. Friedmann; L. Liu; D. Kumar; C. Cesnik;
展开▼
作者单位

展开▼
会议组织
原文格式 PDF
正文语种
中图分类航空;
关键词

相似文献

外文文献
中文文献
专利

1. 带气弹稳定性约束的复合材料浆叶减振优化设计 [J] . 郭俊贤, 向锦武中国航空学报（英文版） . 2004,第003期
2. Composite Rotor Blade Design Optimization for Vibration Reduction with Aeroelastic Constraints [J] . GUO Jun-xian, XIANG Jin-wu Chinese Journal of Aeronautics . 2004,第3期

机译：具有气动弹性约束的减振复合转子叶片设计优化
3. Composite Rotor Blade Design Optimization for Vibration Reduction with Aeroelastic Constraints [J] . GUO Jun-xian, XIANG Jin-wu Chinese journal of aeronautics . 2004,第3期

机译：具有气动弹性约束的减振复合转子叶片设计优化
4. Composite Rotor Blade Design Optimization for Vibration Reduction with Aeroelastic Constraints [J] . GUO Jun-xian, XIANG Jin-wu Chinese journal of aeronautics . 2004,第3期

机译：具有气动弹性约束的减振复合转子叶片设计优化
5. The AVINOR Aeroelastic Simulation Code and Its Application to Reduced Vibration Composite Rotor Blade Design [C] . American Institute of Aeronautics and Astronautics/American Society of Mechanical Engineers/American Society of Civil Engineers/Vertical Flight Technical Society/ASC Structures, Structural Dynamics, and Materials Conference . 2009

机译：Avinor Aeroelastic模拟代码及其在减少振动复合转子叶片设计中的应用
6. Aeroelastic Modeling of Blade Vibration and Its Effect on the Trim and Optimal Performance of Helicopter Rotors Using a Harmonic Balance Approach [D] . Tedesco, Matthew. 2020

机译：叶片振动的气动弹性型造型及其对谐波平衡方法直升机转子的尺寸和最佳性能
7. Fully-coupled aeroelastic simulation with fluid compressibility — For application to vocal fold vibration [O] . Jubiao Yang, Xingshi Wang, Michael Krane, -1

机译：具有流体可压缩性的全耦合气动弹性模拟-用于声带振动
8. Composite Rotor Blade Design Optimization for Vibration Reduction with Aeroelastic Constraints [O] . GUO Jun-xian, XIANG Jin-wu 2004

机译：具有气动弹性约束的减振复合转子叶片设计优化

获取原文

客服邮箱：kefu@zhangqiaokeyan.com

京公网安备：11010802029741号 ICP备案号：京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有

客服微信
服务号