Prediction of rotor blade vortex interaction noise using 3-D unsteady surface pressure

被引：0
|
作者：
机构：
来源：
Hangkong Xuebao | / 6卷 / 723-727期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
相关论文
共 50 条
  • [31] Hovering helicopter rotor blade/vortex interaction noise characteristics in ground effect environment
    Wang, Weiqi
    Chen, Xi
    Zhao, Qijun
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2024, 45 (12):
  • [32] Parallel blade-vortex interaction modelling for helicopter rotor noise control synthesis
    Modini, Sara
    Graziani, Giorgio
    Bernardini, Giovanni
    Gennaretti, Massimo
    INTERNATIONAL JOURNAL OF AEROACOUSTICS, 2014, 13 (7-8) : 587 - 606
  • [33] Active twist smart rotor technology for blade-vortex interaction noise reduction
    Chen, PC
    Baeder, JD
    Evans, RAD
    Niemczuk, J
    Ross, P
    SMART STRUCTURES AND MATERIALS 1999: SMART STRUCTURES AND INTEGRATED SYSTEMS, PTS 1 AND 2, 1999, 3668 : 37 - 49
  • [34] Reduction of helicopter blade-vortex interaction noise by active rotor control technology
    Yu, YH
    Gmelin, B
    Splettstoesser, W
    Philippe, JJ
    Prieur, J
    Brooks, TF
    PROGRESS IN AEROSPACE SCIENCES, 1997, 33 (9-10) : 647 - 687
  • [35] Synthesis of Active Twist Controller for Rotor Blade-Vortex Interaction Noise Alleviation
    Anobile, Alessandro
    Bernardini, Giovanni
    Gennaretti, Massimo
    Testa, Claudio
    JOURNAL OF AIRCRAFT, 2016, 53 (06): : 1865 - 1874
  • [36] Blade-vortex interaction noise reduction with active twist smart rotor technology
    Chen, PC
    Baeder, JD
    Evans, RAD
    Niemczuk, J
    SMART MATERIALS & STRUCTURES, 2001, 10 (01): : 77 - 85
  • [37] HIGHER HARMONIC CONTROL OF A HELICOPTER MODEL ROTOR TO REDUCE BLADE VORTEX INTERACTION NOISE
    SPLETTSTOESSER, WR
    LEHMANN, G
    VANDERWALL, B
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG, 1990, 14 (1-2): : 109 - 116
  • [38] SYNTHESIS OF A ROTOR NOISE CONTROLLER BY PARALLEL BLADE-VORTEX INTERACTION AEROELASTIC MODELLING
    Modini, S.
    Graziani, G.
    Bernardini, G.
    Gennaretti, M.
    ASME PRESSURE VESSELS AND PIPING CONFERENCE - 2014, VOL 4, 2014,
  • [39] MEASUREMENT AROUND A ROTOR BLADE EXCITED IN PITCH .2. UNSTEADY SURFACE PRESSURE
    LAL, MK
    LIOU, SG
    PIERCE, GA
    KOMERATH, NM
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 1994, 39 (02) : 13 - 20
  • [40] Helicopter Blade-Vortex Interaction Airload and Noise Prediction Using Coupling CFD/VWM Method
    Zhao, Yinyu
    Shi, Yongjie
    Xu, Guohua
    APPLIED SCIENCES-BASEL, 2017, 7 (04):
12345