Optimum design for helicopter rotor blades in unsteady aerodynamics system

被引:0
|
作者
Chang, Y.K.
Wang, Y.R.
Hung, C.C.
机构
来源
Transactions of the Aeronautical and Astronautical Society of the Republic of China | 1996年 / 28卷 / 03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] DESIGN OF EXTENDABLE CHORD SECTIONS FOR MORPHING HELICOPTER ROTOR BLADES
    Barbarino, Silvestro
    Gandhi, Farhan
    Webster, Steven D.
    PROCEEDINGS OF THE ASME CONFERENCE ON SMART MATERIALS, ADAPTIVE STRUCTURES AND INTELLIGENT SYSTEMS, 2010, VOL 2, 2010, : 323 - 336
  • [32] NUMERICAL-CALCULATION OF UNSTEADY TRANSONIC POTENTIAL FLOW OVER HELICOPTER ROTOR BLADES
    CARADONNA, FX
    ISOM, MP
    AIAA JOURNAL, 1976, 14 (04) : 482 - 488
  • [33] Deformation Measurements of Helicopter Rotor Blades Using a Photogrammetric System
    Zuo, Chenglin
    Ma, Jun
    Wei, Chunhua
    Yue, Tingrui
    Song, Jin
    PHOTONICS, 2022, 9 (07)
  • [34] Integrated actuation system for individual control of helicopter rotor blades
    Bushko, D
    Fenn, R
    Gerver, M
    Berry, J
    Philips, F
    Merkley, DJ
    SMART STRUCTURES AND INTEGRATED SYSTEMS: SMART STRUCTURES AND MATERIALS 1996, 1996, 2717 : 80 - 90
  • [35] Dynamic Modeling of Helicopter Rotor Blades
    College of Aerospace Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing, 210016, China
    不详
    Tsinghua Sci. Tech., 2009, SUPPL. 2 (84-88):
  • [36] TRANSONIC EFFECTS ON HELICOPTER ROTOR BLADES
    HUBER, H
    MIKULLA, V
    STAHL, H
    VERTICA, 1983, 7 (02): : 87 - 100
  • [37] CHORD MORPHING FOR HELICOPTER ROTOR BLADES
    Riemenschneider, Johannes
    Balzarek, Christoph
    van der Wall, Berend G.
    Majeti, Rohin Kumar
    PREOCEEDINGS OF THE ASME CONFERENCE ON SMART MATERIALS, ADAPTIVE STRUCTURES AND INTELLIGENT SYSTEMS, 2019, 2020,
  • [38] Airfoil design for helicopter rotor blades - A three-dimensional approach
    Hassan, AA
    Charles, BD
    JOURNAL OF AIRCRAFT, 1997, 34 (02): : 197 - 205
  • [39] Multilevel decomposition procedure for efficient design optimization of helicopter rotor blades
    Chattopadhyay, Aditi, 1600, AIAA, Washington, DC, United States (33):
  • [40] Aerodynamics of helicopter rotor in hover: The lifting-vortex line method applied to dihedral tip blades
    Joncheray, P
    AEROSPACE SCIENCE AND TECHNOLOGY, 1997, 1 (01): : 17 - 25