Studies on Digital Shearography for Testing of Aircraft Composite Structures and Honeycomb-based Specimen

被引:6
|
作者
Feng, Huijuan [1 ]
Zhang, Jian [1 ]
Liu, Xiangkai [1 ]
机构
[1] Mil Transportat Univ, Dept Automobile Engn, Tianjin 300161, Peoples R China
来源
FRONTIERS OF MANUFACTURING AND DESIGN SCIENCE II, PTS 1-6 | 2012年 / 121-126卷
关键词
NDT; Shearography; Composite material;
D O I
10.4028/www.scientific.net/AMM.121-126.1264
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper reviews shearography and its applications for testing of aircraft composite structures and honeycomb-based specimen. Shearography is a laser-based interferometry in conjunction with the digital imaging processing technique for full-field measurement of surface deformation. It reveals defects in an object by looking for defect-induced deformation anomalies. It does not require special vibration isolation, and with the development of a small and mobile measuring device (portable inspection system), it can be employed easily in field/factory environments.
引用
收藏
页码:1264 / 1268
页数:5
相关论文
共 50 条
  • [21] MODEL TEST PANEL FOR PROCESSING AND CHARACTERIZATION STUDIES OF HONEYCOMB COMPOSITE STRUCTURES
    ZENG, SY
    SEFERIS, JC
    AHN, KJ
    PEDERSON, CL
    JOURNAL OF ADVANCED MATERIALS, 1994, 25 (02): : 9 - 21
  • [22] Successes and challenges in non-destructive testing of aircraft composite structures
    Hossein TOWSYFYAN
    Ander BIGURI
    Richard BOARDMAN
    Thomas BLUMENSATH
    Chinese Journal of Aeronautics, 2020, 33 (03) : 771 - 791
  • [23] Successes and challenges in non-destructive testing of aircraft composite structures
    Towsyfyan, Hossein
    Biguri, Ander
    Boardman, Richard
    Blumensath, Thomas
    CHINESE JOURNAL OF AERONAUTICS, 2020, 33 (03) : 771 - 791
  • [24] Impact damage in composite aircraft structures - experimental testing and numerical simulation
    Zhang, X
    PROCEEDINGS OF THE INSTITUTION OF MECHANICAL ENGINEERS PART G-JOURNAL OF AEROSPACE ENGINEERING, 1998, 212 (G4) : 245 - 259
  • [25] Successes and challenges in non-destructive testing of aircraft composite structures
    Hossein TOWSYFYAN
    Ander BIGURI
    Richard BOARDMAN
    Thomas BLUMENSATH
    Chinese Journal of Aeronautics , 2020, (03) : 771 - 791
  • [26] Laser-shearography for non-destructive testing of large-area composite helicopter structures
    Pezzoni, R. (r.pezzoni@agusta.it), 2001, British Institute of Non-Destructive Testing (43):
  • [27] A MICROPROCESSOR BASED SYSTEM FOR VIBRATION TESTING OF AIRCRAFT STRUCTURES
    GANESAN, S
    IEEE INSTRUMENTATION AND MEASUREMENT TECHNOLOGY CONFERENCE //: IMTC / PERVASIVE I & M TECHNOLOGY, 1989, : 383 - 387
  • [28] Influences of skin thickness, core topology, depth and direction on flexural deformation and ductile failure of Al honeycomb-based sandwich structures
    Li W.
    Atsushi D.
    Oh Y.H.
    Jirathearanat S.
    Wu Z.A.
    Chua B.W.
    Composites Part B: Engineering, 2022, 239
  • [29] Flexural testing of composite sandwich structures with digital speckle photogrammetry
    Fergusson, A. D.
    Puri, A.
    Morris, A.
    Dear, J. P.
    MODERN PRACTICE IN STRESS AND VIBRATION ANALYSIS VI, PROCEEDINGS, 2006, 5-6 : 135 - +
  • [30] ANALYTICAL AND EXPERIMENTAL STUDIES ON DELAMINATION ARREST FEATURES IN AIRCRAFT COMPOSITE STRUCTURES
    Richard, Luke, I
    Lin, Kuen Y.
    20TH INTERNATIONAL CONFERENCE ON COMPOSITE MATERIALS, 2015,