Review of Damage Tolerance for Composite Sandwich Airframe Structures
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Thomas E. Lacy | Anthony J. Vizzini | J. Tomblin | Bert L. Smith | S. Hooper | J. Tomblin | T. Lacy | A. Vizzini | Bert L. Smith | S. Hooper
[1] Lorna J. Gibson,et al. Failure mode maps for foam core sandwich beams , 1987 .
[2] A. G. Gibson,et al. The static and impact behaviour of polymer composite sandwich beams , 1994 .
[3] D. Cairns,et al. Impact and post-impact response of graphite/epoxy and Kevlar/epoxy structures , 1987 .
[4] Steven G. Russell,et al. Damage Tolerance and Fail-Safety of Composite Sandwich Panels , 1994 .
[5] Michael F. Ashby,et al. The out-of-plane properties of honeycombs , 1992 .
[6] K. S. Wilden,et al. Advanced Technology Composite Fuselage - Manufacturing , 1997 .
[7] Damodar R. Ambur,et al. Response of composite fuselage sandwich side panels subjected to internal pressure and axial tension , 1998 .
[8] Serge Abrate,et al. Localized Impact on Sandwich Structures With Laminated Facings , 1997 .
[9] Damodar R. Ambur,et al. DAMAGE CHARACTERISTICS AND RESIDUAL STRENGTH OF COMPOSITE SANDWICH PANELS IMPACTED WITH AND WITHOUT COMPRESSION LOADING , 1998 .
[10] Alan T. Nettles,et al. Impact testing of glass/phenolic honeycomb panels with graphite/epoxy facesheets , 1990 .
[11] Chun-Gon Kim,et al. Impact Resistance of Composite Laminated Sandwich Plates , 1992 .
[12] Fay,et al. Evaluation of Advanced Sandwich Structure Designed for Improved Durability and Damage Tolerance , 1990 .
[13] Gregory Czarnecki,et al. Damage tolerance of composite sandwich structure , 1995 .
[14] Matthew Claire Taylor. Damage tolerance of composite honeycomb sandwich panels under quasi-static bending and cyclic compression , 1989 .
[15] S. Abrate. Impact on Laminated Composite Materials , 1991 .
[16] B. W. Flynn,et al. Advanced Technology Composite Fuselage - Repair and Damage Assessment Supporting Maintenance , 1997 .
[17] K. E. Simmonds,et al. Low-Velocity Impact Response of Foam-Core Sandwich Composites , 1992 .
[18] Pierre J. A. Minguet,et al. A model for predicting the behavior of impact-damaged minimum gage sandwich panels under compression , 1991 .
[19] L. Lee,et al. Dynamic Responses of Composite Sandwich Plate Impacted by a Rigid Ball* , 1993 .
[20] Paul A. Lagace,et al. Impact Resistance of Composite Sandwich Plates , 1989 .
[21] Ori Ishai,et al. Design of highly damage-tolerant sandwich panels , 1992 .
[22] M. D. Rhodes,et al. Impact fracture of composite sandwich structures , 1975 .
[23] Serge Abrate,et al. Impact on Laminated Composites: Recent Advances , 1994 .
[24] C. Kassapoglou,et al. Compression Strength of Composite Sandwich Structures After Barely Visible Impact Damage , 1996 .
[25] B. F. Backman,et al. Advanced Technology Composite Fuselage: Program Overview , 1997 .
[26] B. W. Flynn,et al. Advanced Technology Composite Fuselage-Structural Performance , 1997 .
[27] B. Z. Jang,et al. Instrumented Impact Testing of Composite Sandwich Panels , 1989 .
[28] C. Sun,et al. Low velocity impact of composite sandwich panels , 1991 .
[29] D R Ambur,et al. Damage-Tolerance Characteristics of Composite Fuselage Sandwich Structures With Thick Facesheets , 1997 .
[30] Ori Ishai,et al. Composite sandwich construction with syntactic foam core: A practical assessment of post-impact damage and residual strength , 1993 .
[31] D. R. Polland,et al. Global Cost and Weight Evaluation of Fuselage Side Panel Design Concepts , 1993 .
[32] C. Kassapoglou,et al. Compressive Strength of Composite Sandwich Panels After Impact Damage: An Experimental and Analytical Study , 1988 .
[33] C. Sun,et al. Indentation Law for Composite Laminates. , 1982 .
[34] Todd K. Saczalski,et al. Advanced experimental design applied to damage tolerance of composite materials , 1991 .
[35] Marshall Rouse,et al. Evaluation of a Composite Sandwich Fuselage Side Panel With Damage and Subjected to Internal Pressure , 1997 .
[36] James Edward Williamson,et al. Response mechanisms in the impact of graphite/epoxy honeycomb sandwich panels , 1991 .
[37] Christos Kassapoglou. Buckling, post-buckling and failure of elliptical delaminations in laminates under compression , 1988 .
[38] William B. Avery,et al. Impact damage resistance of composite fuselage structure, part 1 , 1992 .
[39] Simon Charles Lie,et al. Damage resistance and damage tolerance of thin composite facesheet honeycomb panels , 1989 .