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  • 史勇杰 ( 教授 )

    的个人主页 http://faculty.nuaa.edu.cn/syj/zh_CN/index.htm

  •   教授   博士生导师
  • 招生学科专业:
    航空宇航科学与技术 -- 【招收博士、硕士研究生】 -- 航空学院
    机械 -- 【招收博士、硕士研究生】 -- 航空学院
论文成果 当前位置: 中文主页 >> 科学研究 >> 论文成果
Blade vortex interaction acoustic prediction method for rotor based on aerodynamic/elastic coupling

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所属单位:航空学院
发表刊物:Hangkong Dongli Xuebao
摘要:An engineering method suitable for blade vortex interaction(BVI) airload and acoustic analysis was established based on aerodynamic/elastic coupling. The aerodynamic model includes modified Beddoes wake method and CFD method. Acoustic prediction was based on Ffowcs-Williams Hawkings(FW-H) equation derived by acoustic analogy, and the elastic blade model was based on finite element method. By applying the established models, the airload and acoustic characteristics of rigid operational load survey(OLS) rotor were calculated under BVI flight state firstly, and the validity of the two aerodynamic models was compared, then the influences of elasticity and time step on HART Ⅱ rotor BVI airload and acoustic were analyzed. The results indicate that the time step adopted in BVI calculation should be no more than 2 degree. Peak acoustic pressure of OLS rotor predicted by CFD is only 60% of experimental data because of inherent numerical dissipation, while the modified Beddoes wake method can address this problem with high computation efficiency. Taking blade elasticity into consideration is beneficial for BVI acoustic prediction accuracy. © 2017, Editorial Department of Journal of Aerospace Power. All right reserved.
ISSN号:1000-8055
是否译文:否
发表时间:2017-09-01
合写作者:Wang, Liangquan,徐国华
通讯作者:史勇杰

 

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