Parametric wind tunnel test on rotorcraft aerodynamics and aeroacoustics (Helishape) - test procedures and representative results

被引：0
|
作者：
DLR, Braunschweig, Goettingen, Germany [1 ]
机构：
来源：
Aeronaut J | / 1004卷 / 143-154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
  • [1] A parametric windtunnel test on rotorcraft aerodynamics and aeroacoustics (Helishape) - Test procedures and representative results
    Schultz, KJ
    Splettstoesser, W
    Junker, B
    Wagner, W
    Arnaud, G
    Schoell, E
    Fertis, D
    Mercker, E
    Pengel, K
    AERONAUTICAL JOURNAL, 1997, 101 (1004): : 143 - 154
  • [2] Wind Tunnel Test of a Rotorcraft with Lift Compounding
    Bauknecht, Andre
    Wang, Xing
    Faust, Jan-Arun
    Chopra, Inderjit
    JOURNAL OF THE AMERICAN HELICOPTER SOCIETY, 2021, 66 (01)
  • [3] On cable aerodynamics - Field observation and wind tunnel test
    Matsumoto, M
    Yagi, T
    Sakai, S
    Ohya, J
    Okada, T
    PROCEEDINGS OF THE SECOND INTERNATIONAL SYMPOSIUM ON ADVANCES IN WIND & STRUCTURES (AWAS'02), 2002, : 289 - 296
  • [4] Numerical Simulation of Aerodynamics and Aeroacoustics Wind Tunnel for Whole Vehicle
    Fu Q.
    Yang Z.
    Liang C.
    Liao H.
    Du L.
    Tongji Daxue Xuebao/Journal of Tongji University, 2022, 50 : 107 - 113
  • [5] Inclined cable aerodynamics - wind tunnel test and field observation
    Matsumoto, A
    Yagi, T
    SYSTEM-BASED VISION FOR STRATEGIC AND CREATIVE DESIGN, VOLS 1-3, 2003, : 2345 - 2351
  • [6] Wind tunnel test of rotor aerodynamics with various surface roughness
    Kimura, S.
    Abe, K.
    Iuchi, M.
    Munakata, H.
    European Community Wind Energy Conference, 1990,
  • [7] Smart wing wind tunnel test results
    Scherer, LB
    Martin, CA
    Appa, K
    Kudva, J
    West, MN
    INDUSTRIAL AND COMMERCIAL APPLICATIONS OF SMART STRUCTURES TECHNOLOGIES: SMART STRUCTURES AND MATERIALS 1997, 1997, 3044 : 56 - 66
  • [8] A Parametric Design Method for Hybrid Airfoils for Icing Wind Tunnel Test
    Li, Zhao
    Yang, Guang-jun
    Tong, Xiao-yan
    Jiang, Feng
    INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING, 2021, 2021
  • [9] Investigation of high speed wind tunnel test technology for aerodynamics compensation airspeed heads
    Li, Qi-Chang
    Fan, Kai-Dao
    Wang, Su-Wei
    Liuti Lixue Shiyan yu Celiang/Experiments and Measurements in Fluid Mechanics, 2002, 16 (04):
  • [10] Progressive identification of lateral nonlinear unsteady aerodynamics from wind tunnel test data
    Shuang HU
    Jihong ZHU
    Wei YANG
    ScienceChina(InformationSciences), 2019, 62 (10) : 197 - 199
12345