Barely visible impact damage detection for composite sandwich structures by optical-fiber-based distributed strain measurement
暂无分享,去创建一个
[1] Nobuo Takeda,et al. Smart Composite Sandwich Structures for Future Aerospace Application -Damage Detection and Suppression-: a Review , 2007 .
[3] Nobuo Takeda,et al. Real-time Detection of Debonding between Honeycomb Core and Facesheet using a Small-diameter FBG Sensor Embedded in Adhesive Layer , 2007 .
[4] John S. Tomblin,et al. Impact Damage Characterization and Damage Tolerance of Composite Sandwich Airframe Structures - Phase II , 2002 .
[5] Serge Abrate,et al. Localized Impact on Sandwich Structures With Laminated Facings , 1997 .
[6] Peter H. Bull,et al. Compressive Failure of Impacted NCF Composite Sandwich Panels - Characterisation of the Failure Process , 2004 .
[7] D. Zenkert,et al. Handbook of Sandwich Construction , 1997 .
[8] G. Odegard,et al. Facesheet delamination of composite sandwich materials at cryogenic temperatures , 2006 .
[9] Nobuo Takeda,et al. “Segment-wise model” for theoretical simulation of barely visible indentation damage in composite sandwich beams: Part I – Formulation , 2008 .
[10] Nobuo Takeda,et al. Brillouin spectral response depending on strain non-uniformity within centimeter spatial resolution and its application to internal damage detection in large-scale composite structures , 2008 .
[11] J. Vinson. The Behavior of Sandwich Structures of Isotropic and Composite Materials , 1999 .