Extension of the Lifting Line Model for the Helicopter Rotor.

被引：0
|
作者：
Hille, Ralf
机构：
来源：
Zeitschrift fuer Flugwissenschaften | 1975年 / 23卷 / 03期
关键词：
Compendex;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
HELICOPTERS
引用
收藏
页码：77 / 95
相关论文
共 50 条
  • [41] INFLUENCE OF THE CONTROL LAW ON THE PERFORMANCE OF A HELICOPTER MODEL ROTOR
    DESOPPER, A
    LAFON, P
    CERONI, P
    VERTICA, 1990, 14 (03): : 429 - 437
  • [42] VORTEX MODEL FOR TREATMENT OF FLOW ON ROTOR BLADE OF HELICOPTER
    ISAY, WH
    ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK, 1972, 52 (06): : 283 - &
  • [43] Generic harmonic rotor model for helicopter flight simulation
    1600, (97):
  • [44] MODEL FOR INVESTIGATION OF HELICOPTER FUSELAGE INFLUENCE ON ROTOR FLOWFIELDS
    RAND, O
    GESSOW, A
    JOURNAL OF AIRCRAFT, 1989, 26 (05): : 401 - 402
  • [45] Dynamic model of elastic impact of helicopter rotor blades
    Wang, Yi-Feng
    Wang, Hao-Wen
    Gao, Zheng
    Hangkong Dongli Xuebao/Journal of Aerospace Power, 2009, 24 (09): : 2046 - 2050
  • [46] Simulation model of loads created by a hingeless helicopter rotor
    Girfanov A.M.
    Ledyankina O.A.
    Russian Aeronautics (Iz VUZ), 2015, 58 (2) : 167 - 172
  • [47] EXPERIMENTAL AND ANALYTICAL STUDIES OF A MODEL HELICOPTER ROTOR IN HOVER
    CARADONNA, FX
    TUNG, C
    VERTICA, 1981, 5 (02): : 149 - 161
  • [48] The Application of Snel Stall Model in the Field of Helicopter Rotor
    Liu, Jie
    Chen, Lei
    Zhang, Peng
    Zhao, Peng
    Zhang, Feng
    INTERNATIONAL CONFERENCE ON SUSTAINABLE ENERGY AND ENVIRONMENT PROTECTION (ICSEEP 2015), 2015, : 997 - 1001
  • [49] A GENERIC HARMONIC ROTOR MODEL FOR HELICOPTER FLIGHT SIMULATION
    CHAIMOVICH, M
    ROSEN, A
    RAND, O
    AERONAUTICAL JOURNAL, 1993, 97 (961): : 14 - 24
  • [50] UCA BALANCING DEMONSRTATED ON GAS TURBINE ROTOR.
    Zorz, E.S.
    Martin, M.
    Turbomachinery International, 1987, 28 (06)
12345