Evaluation method for technology maturity of composite aircraft structure

被引：0
|
作者：
Lan, Yuanpei [1 ]
Guan, Zhidong [1 ]
Meng, Qingchun [1 ]
机构：
[1] School of Aeronautic Science and Engineering, Beihang University, Beijing 100191, China
来源：
Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica | 2010年 / 27卷 / 03期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
24
引用
收藏
页码：150 / 154
相关论文
共 50 条
  • [31] The Method of Aircraft Control System Evaluation
    Gruszecki, Jan
    Rogalski, Tomasz
    PROCEEDINGS OF THE ITI 2012 34TH INTERNATIONAL CONFERENCE ON INFORMATION TECHNOLOGY INTERFACES (ITI), 2012, : 429 - 434
  • [32] Fiber/metal composite technology for future primary aircraft structures
    Alderliesten, R.C.
    Benedictus, R.
    Journal of Aircraft, 1600, 45 (04): : 1182 - 1189
  • [33] Fiber/metal composite technology for future primary aircraft structures
    Alderliesten, R. C.
    Benedictus, R.
    JOURNAL OF AIRCRAFT, 2008, 45 (04): : 1182 - 1189
  • [34] Simulation analysis of composite supercharging technology of aircraft piston engines
    Pan, Zhongjian
    He, Qinghua
    Zhang, Xiangjian
    Harbin Gongcheng Daxue Xuebao/Journal of Harbin Engineering University, 2014, 35 (12): : 1543 - 1547
  • [35] Advanced aircraft engine microlaminated intermetallic composite turbine technology
    Rowe, RG
    Skelly, DW
    Jackson, MR
    Larsen, M
    Lachapelle, D
    LAYERED MATERIALS FOR STRUCTURAL APPLICATIONS, 1996, 434 : 3 - 13
  • [36] EVALUATION OF SKELETAL MATURITY BY THE TANNER AND WHITEHOUSE METHOD
    GUIMAREY, LM
    LEJARRAGA, H
    CUSMINSKY, M
    MEDICINA-BUENOS AIRES, 1979, 39 (03) : 312 - 316
  • [37] THE CRASHWORTHINESS DESIGN OF TRANSPORT AIRCRAFT USING COMPOSITE STRUCTURE
    Ren, Yiru
    Xiang, Jinwu
    Zheng, Jianqiang
    20TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS, 2015,
  • [38] Evaluation method of composite insulator aging status based on hyperspectral imaging technology
    Fan, Yihan
    Guo, Yujun
    Liu, Yang
    Xiao, Song
    Zhang, Xueqin
    Wu, Guangning
    MEASUREMENT, 2024, 225
  • [39] High voltage tests on aircraft made in composite structure
    Mikulski, January Lech
    PRZEGLAD ELEKTROTECHNICZNY, 2008, 84 (10): : 16 - 19
  • [40] Optimal composite doubler designs for aluminum aircraft structure
    Spigel, B
    Buckingham, J
    MATERIALS-THE STAR AT CENTER STAGE, 1998, 30 : 12 - 25
12345