Some key issues of aircraft T-Tail flutter calculation

被引：0
|
作者：
Yang, Fei [1 ]
Yang, Zhi-Chun [2 ]
机构：
[1] Strength Department, Shanghai Aircraft Design and Research Institute, Shanghai 200232, China
[2] School of Aeronautics, Northwestern Polytechnical University, Xi'an 710072, China
来源：
Zhendong yu Chongji/Journal of Vibration and Shock | 2011年 / 30卷 / 05期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
13
引用
收藏
页码：136 / 139
相关论文
共 50 条
  • [21] RATIONAL BOUNDS FOR THE T-TAIL AREA
    SOMS, AP
    JOURNAL OF THE AMERICAN STATISTICAL ASSOCIATION, 1980, 75 (370) : 438 - 440
  • [22] Structural optimization technique of a T-tail
    Qiu, Ju
    Sun, Qin
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2013, 227 (G6) : 1009 - 1020
  • [23] Optimization Design of the Supporting Stiffness of T-tail
    Qiu, Ju
    Sun, Qin
    INTERNATIONAL JOINT CONFERENCE ON COMPUTATIONAL SCIENCES AND OPTIMIZATION, VOL 1, PROCEEDINGS, 2009, : 279 - 282
  • [24] Rear fuselage stiffness design of T-tail
    Ju, Qiu
    Qin, Sun
    COMPOSITE STRUCTURES, 2013, 100 : 163 - 172
  • [25] Optimization design for aeroelastic dynamics of T-tail
    Lu, Bin
    Tan, Shengang
    Wan, Zhiqiang
    Yang, Chao
    Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2007, 33 (04): : 409 - 413
  • [26] Rotor wake study near the horizontal tail of a T-tail configuration
    Gorton, SA
    Berry, JD
    Hodges, WT
    Reis, DG
    JOURNAL OF AIRCRAFT, 2002, 39 (04): : 645 - 653
  • [27] LIFTING-SURFACE THEORY FOR AN OSCILLATING T-TAIL
    ISOGAI, K
    AIAA JOURNAL, 1974, 12 (01) : 28 - 37
  • [28] Comprehensive research on vibration characteristics, strength and stability of T-tail
    Ji, Ting-wei
    Zhang, Shuai
    Zhang, Jifa
    JOURNAL OF VIBROENGINEERING, 2015, 17 (04) : 2077 - 2088
  • [29] Mode localization prediction criterion for T-Tail structure
    Yang, Zhichun
    Yang, Fei
    Lixue Xuebao/Chinese Journal of Theoretical and Applied Mechanics, 2010, 42 (02): : 290 - 299
  • [30] INVESTIGATION OF FLUTTERING OF DYNAMICALLY SIMILAR MODEL OF T-TAIL UNIT
    ZIMMERMA.H
    ACHENBAC.E
    ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN, 1969, 17 (11): : 413 - &
12345