GENERIC APPROACH TO DETERMINE OPTIMUM AEROELASTIC CHARACTERISTICS FOR COMPOSITE FORWARD-SWEPT-WING AIRCRAFT - COMMENT

被引：0
|
作者：
WEISSHAAR, TA
机构：
来源：
AIAA JOURNAL | 1985年 / 23卷 / 06期
关键词：
D O I：
10.2514/3.48607
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：978 / 978
页数：1
相关论文
共 23 条
  • [21] Aeroelastic Tailoring of a Composite Forward-Swept Wing Using a Novel Hybrid Pattern Search Method
    Tian, Wei
    Yang, Zhichun
    Gu, Yingsong
    Ouyang, Yan
    JOURNAL OF AEROSPACE ENGINEERING, 2016, 29 (06)
  • [22] SUBSONIC LONGITUDINAL AND LATERAL-DIRECTIONAL CHARACTERISTICS OF A FORWARD-SWEPT-WING FIGHTER CONFIGURATION AT ANGLES OF ATTACK UP TO 47 degree .
    Mann, Michael J.
    Huffman, Jarrett K.
    Fox Jr., Charles H.
    NASA Technical Paper, 1987,
  • [23] STRESS-CONCENTRATION OF THE COMPOSITE-MATERIAL USED BY THE X-29A FORWARD-SWEPT WING AIRCRAFT UNDER VARIOUS TEMPERATURE LEVELS
    YEH, HY
    YEH, HL
    COMPOSITE STRUCTURES 5, 1989, : 535 - 545
123