DURABLE AND DAMAGE-TOLERANT COMPOSITE COMMERCIAL AIRCRAFT STRUCTURE DESIGN APPROACH

被引:1
|
作者
MCCARTY, JE
JOHNSON, RW
机构
来源
JOURNAL OF AIRCRAFT | 1978年 / 15卷 / 01期
关键词
D O I
10.2514/3.58309
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:33 / 39
页数:7
相关论文
共 50 条
  • [1] APPROACH TO DEVELOPMENT OF DURABLE AND DAMAGE TOLERANT COMPOSITE-COMMERCIAL AIRCRAFT STRUCTURE
    MCCARTY, JE
    JOHNSON, RW
    [J]. ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B15 - B15
  • [2] Equivalent level of safety approach to damage-tolerant aircraft structural design
    Lin, KY
    Rusk, DT
    Du, JJ
    [J]. JOURNAL OF AIRCRAFT, 2002, 39 (01): : 167 - 174
  • [3] DAMAGE-TOLERANT DESIGN
    OSGOOD, CC
    [J]. MACHINE DESIGN, 1969, 41 (25) : 91 - &
  • [4] Flutter Failure Risk Assessment for Damage-Tolerant Composite Aircraft Structures
    Styuart, Andrey V.
    Livne, Eli
    Demasi, Luciano
    Mor, Marat
    [J]. AIAA JOURNAL, 2011, 49 (03) : 655 - 669
  • [5] DAMAGE-TOLERANT POLYMER COMPOSITE SYSTEMS
    REIFSNIDER, KL
    [J]. JOURNAL OF METALS, 1988, 40 (11): : 51 - 54
  • [6] DESIGNING FOR DAMAGE-TOLERANT COMPOSITE REPAIRS
    CHIU, WK
    REES, D
    CHALKLEY, P
    JONES, R
    [J]. COMPOSITE STRUCTURES, 1994, 28 (01) : 19 - 37
  • [7] Concept for a damage-tolerant ceramic composite with ''strong'' interfaces
    Tu, WC
    Lange, FF
    Evans, AG
    [J]. JOURNAL OF THE AMERICAN CERAMIC SOCIETY, 1996, 79 (02) : 417 - 424
  • [8] DESIGN AND ANALYSIS OF A COMMERCIAL AIRCRAFT COMPOSITE STRUCTURE
    ERNST, T
    GROTH, C
    MESSMERINGER, T
    MUELLER, G
    [J]. 1989 ANSYS CONFERENCE PROCEEDINGS, VOL 1: ENGINEERING DESIGN OPTIONS : FROM PCS TO PARALLELS, 1989, : B17 - B22
  • [9] Probabilistic risk assessment strategy for damage-tolerant composite spacecraft component structural design
    Knight, NF
    Glaessgen, EH
    Sleight, DW
    [J]. JOURNAL OF SPACECRAFT AND ROCKETS, 2003, 40 (01) : 72 - 82
  • [10] Design and evaluation of a damage-tolerant flight control system
    Hess, RA
    Vetter, TK
    Wells, SR
    [J]. PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 2005, 219 (G4) : 341 - 359