FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W4220876083> ?p ?o ?g. }

• W4220876083 endingPage "2430" @default.
• W4220876083 startingPage "2430" @default.
• W4220876083 abstract "Hat-stringer-stiffened composite panels have been widely used in aircrafts. Accurate failure analysis of them is important for the safety and integrity of the fuselage. During the service period, these panels will bear not only the lateral force caused by the bending of fuselage, but also the radial pressure caused by the internal and external differential pressure during the take-off and landing of the aircraft. However, the latter case lacks investigation. Therefore, experimental and numerical studies for the static and fatigue failure of hat-stringer-stiffened composite panels under four-point bending loading have been performed in this work. To accurately predict the fatigue failure, a novel theoretical model has been proposed based on the fatigue damage theory. In addition, a user-defined subroutine USDFLD is developed for the implementation of the proposed theoretical model in Abaqus. Experimental results show that the main failure modes are the delamination of the skin and debonding between the girder flange and the skin. The experimental average value of the initial debonding load and displacement in static tests are 897.3 N and 10.8 mm, respectively. Predictions exhibit good agreement with experimental results with relative errors within 10%. Experimental average fatigue failure life of the specimens is 33,085 cycles, which is also close to the prediction with relative errors within 10%. This indicates the reliability and applicability of the established theoretical model and numerical method for predicting the failure of hat-shaped girder structures." @default.
• W4220876083 created "2022-04-03" @default.
• W4220876083 creator A5014685734 @default.
• W4220876083 creator A5019952863 @default.
• W4220876083 creator A5044328958 @default.
• W4220876083 creator A5050483499 @default.
• W4220876083 creator A5075889094 @default.
• W4220876083 date "2022-03-25" @default.
• W4220876083 modified "2023-10-18" @default.
• W4220876083 title "Failure Analysis of Hat-Stringer-Stiffened Aircraft Composite Panels under Four-Point Bending Loading" @default.
• W4220876083 cites W1648936407 @default.
• W4220876083 cites W1994380760 @default.
• W4220876083 cites W2000067283 @default.
• W4220876083 cites W2019671295 @default.
• W4220876083 cites W2037021647 @default.
• W4220876083 cites W2038242941 @default.
• W4220876083 cites W2041371113 @default.
• W4220876083 cites W2060372222 @default.
• W4220876083 cites W2074502815 @default.
• W4220876083 cites W2082373049 @default.
• W4220876083 cites W2113196236 @default.
• W4220876083 cites W2152955909 @default.
• W4220876083 cites W2274950976 @default.
• W4220876083 cites W2482338454 @default.
• W4220876083 cites W2534855611 @default.
• W4220876083 cites W2550177320 @default.
• W4220876083 cites W2616913822 @default.
• W4220876083 cites W2681602936 @default.
• W4220876083 cites W2751395246 @default.
• W4220876083 cites W2765988778 @default.
• W4220876083 cites W2899029914 @default.
• W4220876083 cites W2980038262 @default.
• W4220876083 cites W2985751965 @default.
• W4220876083 cites W3004657228 @default.
• W4220876083 cites W3014852737 @default.
• W4220876083 cites W3080266656 @default.
• W4220876083 cites W3084186411 @default.
• W4220876083 cites W3093010580 @default.
• W4220876083 cites W3119562872 @default.
• W4220876083 doi "https://doi.org/10.3390/ma15072430" @default.
• W4220876083 hasPubMedId "https://pubmed.ncbi.nlm.nih.gov/35407760" @default.
• W4220876083 hasPublicationYear "2022" @default.
• W4220876083 type Work @default.
• W4220876083 citedByCount "20" @default.
• W4220876083 countsByYear W42208760832022 @default.
• W4220876083 countsByYear W42208760832023 @default.
• W4220876083 crossrefType "journal-article" @default.
• W4220876083 hasAuthorship W4220876083A5014685734 @default.
• W4220876083 hasAuthorship W4220876083A5019952863 @default.
• W4220876083 hasAuthorship W4220876083A5044328958 @default.
• W4220876083 hasAuthorship W4220876083A5050483499 @default.
• W4220876083 hasAuthorship W4220876083A5075889094 @default.
• W4220876083 hasBestOaLocation W42208760831 @default.
• W4220876083 hasConcept C104779481 @default.
• W4220876083 hasConcept C113556839 @default.
• W4220876083 hasConcept C127313418 @default.
• W4220876083 hasConcept C127413603 @default.
• W4220876083 hasConcept C151730666 @default.
• W4220876083 hasConcept C159985019 @default.
• W4220876083 hasConcept C18747710 @default.
• W4220876083 hasConcept C192562407 @default.
• W4220876083 hasConcept C196316656 @default.
• W4220876083 hasConcept C2778417280 @default.
• W4220876083 hasConcept C2778843982 @default.
• W4220876083 hasConcept C30239060 @default.
• W4220876083 hasConcept C58097730 @default.
• W4220876083 hasConcept C66938386 @default.
• W4220876083 hasConcept C77928131 @default.
• W4220876083 hasConcept C87210426 @default.
• W4220876083 hasConceptScore W4220876083C104779481 @default.
• W4220876083 hasConceptScore W4220876083C113556839 @default.
• W4220876083 hasConceptScore W4220876083C127313418 @default.
• W4220876083 hasConceptScore W4220876083C127413603 @default.
• W4220876083 hasConceptScore W4220876083C151730666 @default.
• W4220876083 hasConceptScore W4220876083C159985019 @default.
• W4220876083 hasConceptScore W4220876083C18747710 @default.
• W4220876083 hasConceptScore W4220876083C192562407 @default.
• W4220876083 hasConceptScore W4220876083C196316656 @default.
• W4220876083 hasConceptScore W4220876083C2778417280 @default.
• W4220876083 hasConceptScore W4220876083C2778843982 @default.
• W4220876083 hasConceptScore W4220876083C30239060 @default.
• W4220876083 hasConceptScore W4220876083C58097730 @default.
• W4220876083 hasConceptScore W4220876083C66938386 @default.
• W4220876083 hasConceptScore W4220876083C77928131 @default.
• W4220876083 hasConceptScore W4220876083C87210426 @default.
• W4220876083 hasFunder F4320321001 @default.
• W4220876083 hasFunder F4320335787 @default.
• W4220876083 hasIssue "7" @default.
• W4220876083 hasLocation W42208760831 @default.
• W4220876083 hasLocation W42208760832 @default.
• W4220876083 hasLocation W42208760833 @default.
• W4220876083 hasOpenAccess W4220876083 @default.
• W4220876083 hasPrimaryLocation W42208760831 @default.
• W4220876083 hasRelatedWork W2051478696 @default.
• W4220876083 hasRelatedWork W2124672486 @default.
• W4220876083 hasRelatedWork W2318836800 @default.
• W4220876083 hasRelatedWork W2412505016 @default.
• W4220876083 hasRelatedWork W2546418446 @default.

• next