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2010, 1. Aufl., Aerospace Series, ISBN 9781600867804, xiv, 300
Design and Analysis of Composite Structures enables graduate students and engineers to generate meaningful and robust designs of complex composite structures.... 
Airframes | Mechanical engineering & materials | Technology | Aeronautics & Astronautics | Composite construction | Structural engineering
Book
Journal of Composite Materials, ISSN 0021-9983, 12/2016, Volume 50, Issue 30, pp. 4307 - 4317
An approach to predict static and fatigue failure of composite laminates with holes is presented. Static failure is predicted when the stress averaged over a... 
composite laminates | Fatigue | strength | holes | impact | BEHAVIOR | CIRCULAR HOLE | MATERIALS SCIENCE, COMPOSITES | MODEL | FAILURE | PREDICTION | FRACTURE | PLATE | LIFE
Journal Article
Journal of Aircraft, ISSN 0021-8669, 05/2014, Volume 51, Issue 3, pp. 833 - 840
The increased use of composites in airframe structures creates some very challenging design problems where the need for low weight and low, or at least... 
COMBINED INPLANE | LAP JOINTS | ENGINEERING, AEROSPACE | Usage | Composite materials | Design engineering | Cost control | Aerospace engineering | Aircraft components | Airframes | Low weight | Fuselages | Aircraft | Joints | Optimization
Journal Article
Composites Part A, ISSN 1359-835X, 2010, Volume 41, Issue 5, pp. 663 - 669
A method to predict fatigue of composites under spectrum loading is proposed. It is based on a recently developed approach for constant amplitude loading where... 
B. Strength | C. Analytical modelling | A. Laminate | B. Fatigue | Laminate | Fatigue | MATERIALS SCIENCE, COMPOSITES | ENGINEERING, MANUFACTURING | Analytical modelling | LIFE PREDICTION | Strength | DAMAGE MODEL
Journal Article
Composites Part A, ISSN 1359-835X, 10/2017, Volume 101, pp. 381 - 393
Journal Article
Composites Science and Technology, ISSN 0266-3538, 06/2014, Volume 98, pp. 28 - 35
An approach to obtain accurate estimates of the compression after impact strength of quasi-isotropic composite laminates is presented. The method makes use of... 
C. Modeling | B. Impact behavior | A. Laminate | INVERSE METHOD | TENSILE STIFFNESS | Laminate | MATERIALS SCIENCE, COMPOSITES | Impact behavior | MODEL | Modeling | DAMAGE | Laminated materials | Analysis | Stresses | Impact strength | Mathematical models | Compressive strength | Damage | Laminates | Inclusions | Failure
Journal Article
2015, 1, Aerospace series, ISBN 1119013216, 256
Comprehensively covers new and existing methods for the design and analysis of composites structures with damage present Provides efficient and accurate... 
Design | Composite materials | Structural analysis | Construction Engineering | Composite construction | Strains and stresses
eBook
Journal of composite materials, ISSN 1530-793X, 2018, Volume 53, Issue 4, pp. 425 - 443
An energy method based on beam theory is proposed to determine the strain energy release rate of an existing crack in composite laminates. The developed... 
delamination | Laminate | composite beam | energy release rate | DCB | DOUBLE-CANTILEVER BEAM | CRACK-PROPAGATION | MATERIALS SCIENCE, COMPOSITES | MIXED-MODE DELAMINATION | INTERFACE | GROWTH | SEPARATION | FRACTURE-MECHANICS
Journal Article
Journal of Composite Materials, ISSN 0021-9983, 11/2007, Volume 41, Issue 22, pp. 2737 - 2754
An approach to construct the stress (or load) vs. cycles curve for composite structures under constant amplitude loading is presented. The approach is based on... 
Constant amplitude | Fatigue | Composites | Probability of failure | composites | CARBON-FIBER COMPOSITES | fatigue | DESIGN | probability of failure | BEHAVIOR | MATERIALS SCIENCE, COMPOSITES | MODEL | STRESS | constant amplitude | DAMAGE
Journal Article
Applied Composite Materials, ISSN 0929-189X, 8/2017, Volume 24, Issue 4, pp. 945 - 963
...Repair of Composites: Design Choices Leading to Lower Life-Cycle Cost Christos Kassapoglou 1 & Konstantin Rangelov 2 & Svilen Rangelov 2 Received: 11 November... 
Polymer Sciences | Materials Science | Stiffened panel | Classical Mechanics | Characterization and Evaluation of Materials | Industrial Chemistry/Chemical Engineering | Repair | Cost | Modular structure | SIZE | MATERIALS SCIENCE, COMPOSITES | JOINTS | Aircraft components | Modules | Maintenance | Cost analysis | Damage | Aircraft structures | Wing panels | Assembly | Life cycle costs | Aging aircraft
Journal Article
Composite structures, ISSN 0263-8223, 2019, Volume 211, pp. 89 - 99
A fibre placement architecture, Advanced Placed Ply (AP-PLY), has been shown to give significantly improved damage tolerance characteristics of composite... 
Energy release rate | Delamination | Optimization | AP-PLY composite laminates | DCB | FRACTURE-TOUGHNESS | STRESS INTENSITY FACTORS | MATERIALS SCIENCE, COMPOSITES | SIMULATION | DAMAGE | COHESIVE ZONE MODEL | FAILURE ANALYSIS | ENERGY-RELEASE RATE | FATIGUE-CRACK GROWTH | PROPAGATION | Laminated materials | Analysis
Journal Article
Thin-walled structures, ISSN 0263-8231, 2017, Volume 119, pp. 235 - 246
Grid stiffened panels promise increased damage tolerance with reduced weight. Recent progress in automated manufacturing of composites has made it possible to... 
Composites | Manufacturing | Grid structures | Failure | Impact damage | ENGINEERING, CIVIL | Analysis | Composite materials industry | Aerospace engineering
Journal Article
06/2013, 2, Aerospace series, ISBN 1118536940, 410
New edition updated with additional exercises and two new chapters. Design and Analysis of Composite Structures: With Applications to Aerospace Structures, 2nd... 
Mechanical Engineering | Structural engineering | Airframes | Composite construction | Materials
eBook
Structural and Multidisciplinary Optimization, ISSN 1615-147X, 6/2014, Volume 49, Issue 6, pp. 931 - 952
Journal Article
Composites Part B, ISSN 1359-8368, 05/2014, Volume 61, pp. 116 - 126
An efficient method to determine the type, size, and location of damage in impacted quasi-isotropic composite laminates is presented. The method uses the peak... 
C. Analytical modeling | B. Impact behavior | LOW-VELOCITY IMPACT | GRAPHITE EPOXY | Analytical modeling | MATERIALS SCIENCE, COMPOSITES | INTERLAMINAR STRESSES | PLATES | MASS IMPACT | PREDICTION | ENGINEERING, MULTIDISCIPLINARY | TRANSIENT-RESPONSE | SUBJECT | Impact behavior | LOADS | Laminated materials | Analysis
Journal Article
Composites Part A, ISSN 1359-835X, 2008, Volume 39, Issue 1, pp. 104 - 112
A new concept for designing composite panels with improved performance under compression is presented. In this concept, the panel consists of two different... 
C. Analytical modelling | B. Stress concentrations | B. Buckling | A. Laminates | analytical modelling | SHEAR | buckling | stress concentrations | STACKING-SEQUENCE | VIBRATION | MATERIALS SCIENCE, COMPOSITES | OPTIMIZATION | ENGINEERING, MANUFACTURING | laminates | GENETIC ALGORITHM
Journal Article
CEAS aeronautical journal, ISSN 1869-5590, 2018, Volume 10, Issue 2, pp. 403 - 417
...: effect of various design choices Gunther Moors 1 · Christos Kassapoglou 1 · Sergio Frascino Müller de Almeida 2 · Clovis Augusto Eça Ferreira 3 Received: 17 February... 
Engineering | Skin buckling | Mass/weight estimation | Composite wing-box design | Post-buckling | Aircraft design | Stiffener buckling | Composite structures | Aerospace Technology and Astronautics | Buckling | Trade studies
Journal Article
Journal of Reinforced Plastics and Composites, ISSN 0731-6844, 10/2015, Volume 34, Issue 19, pp. 1603 - 1614
A numerical simulation is established to model low-speed impact damage of composite plates. A combination of the Hashin, and Puck failure criteria along with... 
Impact | Composites | Compression | Simulation | Damage | damage | LOW-VELOCITY IMPACT | DELAMINATION | POLYMER SCIENCE | EFFICIENT APPROACH | simulation | MATERIALS SCIENCE, COMPOSITES | STRENGTH | COHESIVE INTERFACE ELEMENTS | composites | LAMINATED COMPOSITES | SUBJECT | compression | FIBER-COMPOSITES
Journal Article
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