Add to ORKGProgressive failure analyses results are presented for composite panels with and without a cutout and subjected to in-plane shear loading and compression loading well into their postbuckling regime. Ply damage modes such as matrix cracking, fiber-matrix shear, and fiber failure are modeled by degrading the material properties. Results from finite element analyses are compared with experimental data. Good agreement between experimental data and numerical results are observed for most structural configurations when initial geometric imperfections are appropriately modeled
The ability to predict the structural response of composites offers a significant advantage to desig...
A new progressive failure analysis capability for stiffened composite panels has been developed base...
Aircraft composites structures are typically made using stiffened skin construction as it provides a...
Progressive failure analyses results are presented for composite panels with and without a cutout an...
Experimental and analytical results are presented for progressive failure of stiffened composite pan...
A progressive failure methodology is developed and demonstrated to simulate the initiation and mater...
AbstractA mechanism-based progressive failure analyses (PFA) approach is developed for fiber reinfor...
This article presents a finite element-based study of geometrically non-linear progressive failure a...
A methodology for analysing the degradation and collapse in postbuckling composite structures is pro...
A research on the progressive damage analysis subjected to tensile load for woven composite plates i...
This paper is concerned with the development of a failure initiation and progressive failure analysi...
The objective of this research was to determine the physical response, including material failure, o...
The increasing use of composite materials for commercial aircrafts has encouraged research activitie...
The damage tolerance properties of a composite sandwich structure are investigated with a Progressiv...
The behavior and strength of carbon ber reinforced polymer (CFRP) panels subjected\ud to tensile loa...
The ability to predict the structural response of composites offers a significant advantage to desig...
A new progressive failure analysis capability for stiffened composite panels has been developed base...
Aircraft composites structures are typically made using stiffened skin construction as it provides a...
Progressive failure analyses results are presented for composite panels with and without a cutout an...
Experimental and analytical results are presented for progressive failure of stiffened composite pan...
A progressive failure methodology is developed and demonstrated to simulate the initiation and mater...
AbstractA mechanism-based progressive failure analyses (PFA) approach is developed for fiber reinfor...
This article presents a finite element-based study of geometrically non-linear progressive failure a...
A methodology for analysing the degradation and collapse in postbuckling composite structures is pro...
A research on the progressive damage analysis subjected to tensile load for woven composite plates i...
This paper is concerned with the development of a failure initiation and progressive failure analysi...
The objective of this research was to determine the physical response, including material failure, o...
The increasing use of composite materials for commercial aircrafts has encouraged research activitie...
The damage tolerance properties of a composite sandwich structure are investigated with a Progressiv...
The behavior and strength of carbon ber reinforced polymer (CFRP) panels subjected\ud to tensile loa...
The ability to predict the structural response of composites offers a significant advantage to desig...
A new progressive failure analysis capability for stiffened composite panels has been developed base...
Aircraft composites structures are typically made using stiffened skin construction as it provides a...