Effects of wing and canard sweep on lift enhancement of canard configurations

被引：0
|
作者：
机构：
[1] [1,Ma, Bao-Feng
[2] 1,Liu, Pei-Qing
[3] 1,Wei, Yuan
来源：
Ma, B.-F. (BaofengMa@hotmail.com) | 1600年 / American Institute of Aeronautics and Astronautics Inc.卷 / 41期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
21
引用
收藏
相关论文
共 50 条
  • [41] NUMERICAL TECHNIQUE FOR SUBSONIC FLOWS PAST 3 DIMENSIONAL CANARD-WING CONFIGURATIONS WITH EDGE SEPARATIONS
    KANDIL, OA
    MOOK, DT
    NAYFEH, AH
    ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B7 - B7
  • [42] CANARD-WING SHAPE OPTIMIZATION WITH AERODYNAMIC REQUIREMENTS
    DESILVA, BME
    CARMICHAEL, RL
    JOURNAL OF AIRCRAFT, 1978, 15 (11): : 705 - 706
  • [43] Canard-wing interference effects on the flight characteristics of a transonic passenger aircraft
    Ghoreyshi, Mehdi
    Darragh, Ryan
    Harrison, Sean
    Lofthouse, Andrew J.
    Hamlington, Peter E.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 69 : 342 - 356
  • [44] Effect of Canard to the Aerodynamic Characteristics of Blended Wing Body Airplane
    Ali, Zurriati Mohd
    Kuntjoro, Wahyu
    Wisnoe, Wirachman
    IEEE SYMPOSIUM ON BUSINESS, ENGINEERING AND INDUSTRIAL APPLICATIONS (ISBEIA 2012), 2012, : 696 - 700
  • [45] The influence of canard wing parameters on the vertical water entry of a vehicle
    Li, Wenpeng
    Wang, Cong
    Wei, Yingjie
    Ding, Yanyi
    Bao, Jian
    PHYSICS OF FLUIDS, 2024, 36 (12)
  • [46] Aspects of canard-wing vortices interaction in subsonic flow
    Department of Mechanical and Aerospace Engineering, Science and Research Branch, Islamic Azad University, Poonak, Tehran, Iran
    不详
    不详
    Sci. Iran., 3 (743-754):
  • [47] AN ANALYTICAL STUDY OF THE INDUCED DRAG OF CANARD-WING-TAIL AIRCRAFT CONFIGURATIONS WITH VARIOUS LEVELS OF STATIC STABILITY
    BUTLER, GF
    AERONAUTICAL JOURNAL, 1983, 87 (868): : 293 - 300
  • [48] AERODYNAMIC DESIGN OPTIMIZATION TRIM ANALYSIS OF CANARD CONVENTIONAL CONFIGURATIONS
    KEITH, MW
    SELBERG, BP
    JOURNAL OF AIRCRAFT, 1984, 21 (03): : 183 - 192
  • [49] Experimental investigation on the effects of the height of distant canard wing of a forward-swept configuration
    Zhan, Jingxia
    Wang, Jinjun
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2005, 31 (09): : 994 - 998
  • [50] Rotor design for the performance optimization of Canard Rotor/Wing aircraft
    Lee, JW
    Jeon, KS
    Kim, MJ
    Byun, YH
    Kim, CJ
    Yu, YH
    COMPUTATIONAL SCIENCE AND ITS APPLICATIONS - ICCSA 2006, PT 5, 2006, 3984 : 932 - 941
12345