ACTIVE AIRPLANE WING SYSTEM

被引：0
作者：
不详
机构：
来源：
COMPRESSED AIR | 1972年 / 77卷 / 03期
关键词：
D O I：
暂无
中图分类号：
T [工业技术];
学科分类号：
08 ;
摘要：
引用
收藏
页码：14 / &
相关论文
共 50 条
  • [21] OPTIMIZATION OF AIRPLANE WING STRUCTURES UNDER TAXIING LOADS
    RAO, SS
    COMPUTERS & STRUCTURES, 1987, 26 (03) : 469 - 479
  • [22] Multi-functional active noise control system on headrest of airplane seat
    Chang, Cheng-Yuan
    Chuang, Chia-Tseng
    Kuo, Sen M.
    Lin, Chia-Hao
    MECHANICAL SYSTEMS AND SIGNAL PROCESSING, 2022, 167
  • [23] Shape-Shifting Airplane Wing for More Energy Efficiency
    朱盛榕
    热能动力工程, 2019, 34 (11) : 7 - 7
  • [24] ABOUT LARGE U SHAPE WING OF GLIDER AIRPLANE MODEL
    Arghir, George
    ACTA TECHNICA NAPOCENSIS SERIES-APPLIED MATHEMATICS MECHANICS AND ENGINEERING, 2019, 62 (01): : 19 - 22
  • [25] MEASURING SURFACE GEOMETRY OF AIRPLANE WING BY MEANS OF TWO METHODS
    Brucas, Domantas
    Suziedelyte-Visockiene, Jurate
    AVIATION, 2009, 13 (02) : 44 - 49
  • [26] THEORY OF AIRPLANE WING PROFILES IN EXPONENTIAL SHEAR-FLOW
    WEISSINGER, J
    INGENIEUR ARCHIV, 1968, 37 (01): : 10 - +
  • [27] Nondestructive testing of commercial airplane composite wing tip components
    Little, Mark L., 2000, SAMPE, Covina, CA, United States (45):
  • [28] STEP BY STEP DESIGN OF AN AIRPLANE WING FOR MINIMUM WEIGHT.
    Patel, T.S.
    Trabelsi, S.B.
    Al-Colfat, A.A.
    Modelling, simulation & control. B, 1987, 11 (02): : 55 - 64
  • [29] Airplane wings - Influence of the form at the end of the wing on marginal phenomena
    Valensi, J
    COMPTES RENDUS HEBDOMADAIRES DES SEANCES DE L ACADEMIE DES SCIENCES, 1936, 203 : 489 - 492
  • [30] Control of wing for micro-airplane with smart material and laser
    Kajiwara, I
    Ishikawa, H
    Furuya, S
    Yabe, T
    Nishidome, C
    BEAMED ENERGY PROPULSION, 2003, 664 : 545 - 556
12345