中文
  • 陈希
  • 直升机动力学全国重点实验室/直升机研究院
 

Educational Experience

  • 2001.92004.6

     安徽师范大学附属中学   理科   无学位   普通高中毕业 

  • 2004.92008.7

     南京航空航天大学   飞行器环境控制与生命保障工程   Bachelor's Degree in Engineering   University graduated 

  • 2011.92019.1

     南京航空航天大学   飞行器设计   Doctoral Degree in Engineering   With Certificate of Graduation for Doctorate Study 

Research Group

  • 新型旋翼气动及噪...

    团队依托直升动力...

Social Affiliations

  • 2023.2Now

    《气动研究与试验》期刊 青年编委

  • 2023.5Now

    中国航空学会结冰与防除冰分会 青年委员

Research Focus

  • [1] 直升机CFD

  • [2] 直升机结冰预测

  • [3] 旋翼气动噪声

  • [4] 直升机空气动力学

 

Personal Information

陈希,南京航空航天大学直升机动力学全国重点实验室,讲师(院聘副研究员),硕士生导师。2004年以来一直在南京航空航天大学学习,获飞行器设计专业工学博士,其中2017~2018年赴英国Glasgow大学航空系访问研究。

长期从事直升机气动声学、直升机CFD、直升机结冰、直升机空气动力学领域的科研工作,先后主持了国防173课题、专题、陆航预研、旋翼专项等国家级项目,在《AIAA Journal》、《Journal of Aircraft》、《Aerospace Science and Technology》等国际著名学术期刊及会议上发表学术论文70余篇,其中SCI、EI收录40余篇,授权发明专利40余项担任AST、JSV、CJA、航空学报等期刊审稿人,获国防科技进步一等奖1项(排3)

ScopusORCID部分论文与发明专利(10项):

1. Chen Xi, Zhao Qijun, George N. Barakos. Numerical analysis of aerodynamic characteristics of iced rotor in forward flight. AIAA Journal, 2019, 57(4): 1523-1537. (SCI, EI)

2. Chen Xi, Zhang Kai, Zhao Qijun, Wang Weiqi. Numerical analysis of rotor aeroacoustic characteristics during collective pitch aperiodic variation in hover. Aerospace Science and Technology, 2022, 21(8):731-765. (SCI, EI)

3. Chen Xi, Zhao Qijun. Computational investigations of water collection efficiency on blades in unsteady vortex flowfield of rotor. Aerospace Science and Technology, 2018, 79: 482-491. (SCI, EI)

4. Chen Xi, Zhao Qijun. Numerical simulations for ice accretion on rotors using new three-dimensional icing model. Journal of Aircraft, 2017, 54(4):1428-1442. (SCI, EI)

5. Bao Weicheng, Wang Weiqi, Chen Xi, Zhao Qijun. Numerical analyses of aeroacoustic characteristics of tiltrotor considering the aerodynamic interaction by the fuselage in hover. Aerospace Science and Technology, 2023, 141, 108558. (SCI, EI,通讯作者,学生一作)

6. Wang Weiqi, Cui Zhuangzhuang, Chen Xi, Zhao Qijun. A novel efficient calculation method for rotor aeroacoustic characteristics based on multiple aerodynamic surfaces source model. Applied Acoustics, 2024, 225:596-620. (SCI, EI,通讯作者,学生一作)

7. Xu Hang, Wang Weiqi, Chen Xi, Zhao Qijun. Numerical analysis of aeroacoustic characteristics for coaxial counter rotating propellers considering the self-interference effect, Aerospace Science and Technology, 2024, 109358. (SCI, EI,通讯作者,学生一作)

8. Yang Tao, Sun Dazhi, Zhao Qijun, Zhao Guoqing, Chen Xi. Perturbed polynomial reconstructed seventh-order hybrid WENO scheme with improved accuracy and resolution. Computers and Fluids, 2025, 106548. (SCI, EI,通讯作者,学生一作)

9. 一种降噪桨尖结构、应用其的直升机及直升机的降噪方法,发明专利,第一发明人

10. 一种旋翼气动噪声的计算方法及系统,发明专利,第一发明人




  • Gender:Male
  • Alma Mater:南京航空航天大学
  • Business Address:明故宫校区A5楼219
  • Contact Information:chenxicc@nuaa.edu.cn
  • E-Mail:
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