Predictions on the Internal Loads and Structural Deflection in a Full-scale Experimental Bearingless Rotor

被引：0

作者：

Eun, WongJong ^{[1
]}

Ryu, HanYeol ^{[1
]}

Shin, SangJoon ^{[2
]}

Kee, YoungJung ^{[3
]}

Kim, Deog-Kwan ^{[3
]}

机构：

[1] Seoul Natl Univ, Dept Aerosp Engn, Seoul 151744, South Korea

[2] Seoul Natl Univ, Inst Adv Aerosp Technol, Dept Aerosp Engn, Seoul 151744, South Korea

[3] Korea Aerosp Res Inst, Taejon 305806, South Korea

来源：

INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | 2015年 / 16卷 / 01期

基金：

新加坡国家研究基金会;

关键词：

Bearingless Rotor; Aeromechanical Analysis; Rotorcraft Comprehensive Analysis;

D O I：

10.5139/IJASS.2015.16.1.110

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this paper, the unsteady aerodynamics and blade structural dynamics of an experimental bearingless rotor were analyzed. Due to the multiple load path and nonlinear behavior of a bearingless rotor, sophisticated structural modeling and structural-aerodynamic coupled analysis is required. To predict the internal load and deformation of an experimental bearingless rotor, trim analysis was implemented. The results showed good agreement when compared with those predicted by CAMRAD II the rotorcraft comprehensive analysis. It is possible to extend the present structural-aerodynamic combined analysis to further advanced configurations of the bearingless rotor in the future.

引用

页码：110 / 122

页数：13

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