Matches in SemOpenAlex for { <https://semopenalex.org/work/W2883005027> ?p ?o ?g. }
Showing items 1 to 65 of
65
with 100 items per page.
- W2883005027 abstract "Application of a flexural or bending load on a Carbon fiber reinforced polymer(CFRP) specimenleads to both tensile and compressive stress state across the thickness of the specimen thereby resultingin a more complex damage behavior as the tensile and compressive failure modes of a compositematerial are different. Study of damage behavior of specimen includes location of damage initiation,damage propagation, various types damage modes and their interactions, prediction of damageinitiation load and final failure load. Damage behavior of the CFRP specimen has to be studiedfor its efficient and sustainable design. In the present thesis, damage behavior of pristine CFRPspecimen (without hole), specimen with both single circular hole and multiple circular holes havingthree different configurations (two hole longitudinal (2HL), two hole transverse (2HT) and two holediagonal (2HD)) was studied both experimentally and numerically under four point flexural loading.The layup sequence of the CFRP specimen having Unidirectional (UD) [0]16 and Quasi-isotropic[−45/0/45/90]2s are studied. Two-dimensional Digital Image correlation(DIC) technique was employedfor capturing the in-plane displacement and strains across the thickness of the specimen.Finite element (FE) based Progressive damage analysis(PDA) the CFRP specimen was performed.In the progressive damage model, Hashin’s failure criteria was implemented for the predictionof damage initiation of both fiber or matrix at a lamina level, material property degradationmodel was implemented for modelling damage evolution in the specimen and cohesive zone modelwas implemented for predicting the intiation and propagation of interlaminar delamination betweenlayers of the specimen. Damage behavior of the specimen obtained from experiment was comparedwith the results obtained from PDM for validation. Additionally, the variation of load vs displacement,longitudinal strain distribution over the thickness face of the CFRP specimen obtained bothexperimentally and numerically were studied and the corresponding plots obtained from both werecompared.Finally, the load carrying capacity of pristine specimen, specimen with single hole andspecimen with multiple holes with three different configurations (2HL,2HT and 2HD) were comparedand it was also seen which type of specimen according to the two lay up sequences which areunidirectional [0]16 and Quasi [−45/0/45/90]2s was more stiffer and stronger" @default.
- W2883005027 created "2018-08-03" @default.
- W2883005027 creator A5075847263 @default.
- W2883005027 creator A5085427673 @default.
- W2883005027 date "2018-01-01" @default.
- W2883005027 modified "2023-09-27" @default.
- W2883005027 title "Progressive damage analysis of CFRP Laminatewith circular cutouts under flexural loading" @default.
- W2883005027 hasPublicationYear "2018" @default.
- W2883005027 type Work @default.
- W2883005027 sameAs 2883005027 @default.
- W2883005027 citedByCount "0" @default.
- W2883005027 crossrefType "dissertation" @default.
- W2883005027 hasAuthorship W2883005027A5075847263 @default.
- W2883005027 hasAuthorship W2883005027A5085427673 @default.
- W2883005027 hasConcept C112950240 @default.
- W2883005027 hasConcept C127413603 @default.
- W2883005027 hasConcept C135628077 @default.
- W2883005027 hasConcept C154954056 @default.
- W2883005027 hasConcept C159985019 @default.
- W2883005027 hasConcept C178405089 @default.
- W2883005027 hasConcept C192562407 @default.
- W2883005027 hasConcept C2778969670 @default.
- W2883005027 hasConcept C2781072879 @default.
- W2883005027 hasConcept C66938386 @default.
- W2883005027 hasConcept C86060186 @default.
- W2883005027 hasConcept C87210426 @default.
- W2883005027 hasConceptScore W2883005027C112950240 @default.
- W2883005027 hasConceptScore W2883005027C127413603 @default.
- W2883005027 hasConceptScore W2883005027C135628077 @default.
- W2883005027 hasConceptScore W2883005027C154954056 @default.
- W2883005027 hasConceptScore W2883005027C159985019 @default.
- W2883005027 hasConceptScore W2883005027C178405089 @default.
- W2883005027 hasConceptScore W2883005027C192562407 @default.
- W2883005027 hasConceptScore W2883005027C2778969670 @default.
- W2883005027 hasConceptScore W2883005027C2781072879 @default.
- W2883005027 hasConceptScore W2883005027C66938386 @default.
- W2883005027 hasConceptScore W2883005027C86060186 @default.
- W2883005027 hasConceptScore W2883005027C87210426 @default.
- W2883005027 hasLocation W28830050271 @default.
- W2883005027 hasOpenAccess W2883005027 @default.
- W2883005027 hasPrimaryLocation W28830050271 @default.
- W2883005027 hasRelatedWork W1502296169 @default.
- W2883005027 hasRelatedWork W1573135615 @default.
- W2883005027 hasRelatedWork W1792672662 @default.
- W2883005027 hasRelatedWork W2034303660 @default.
- W2883005027 hasRelatedWork W2201640747 @default.
- W2883005027 hasRelatedWork W2238406051 @default.
- W2883005027 hasRelatedWork W2246631664 @default.
- W2883005027 hasRelatedWork W2309000007 @default.
- W2883005027 hasRelatedWork W2320790558 @default.
- W2883005027 hasRelatedWork W2326748536 @default.
- W2883005027 hasRelatedWork W2742607441 @default.
- W2883005027 hasRelatedWork W277293756 @default.
- W2883005027 hasRelatedWork W2966148218 @default.
- W2883005027 hasRelatedWork W2973305220 @default.
- W2883005027 hasRelatedWork W2999279502 @default.
- W2883005027 hasRelatedWork W3091761750 @default.
- W2883005027 hasRelatedWork W3127946198 @default.
- W2883005027 hasRelatedWork W3162519245 @default.
- W2883005027 hasRelatedWork W3166476301 @default.
- W2883005027 hasRelatedWork W2400582981 @default.
- W2883005027 isParatext "false" @default.
- W2883005027 isRetracted "false" @default.
- W2883005027 magId "2883005027" @default.
- W2883005027 workType "dissertation" @default.