FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W1566016654> ?p ?o ?g. }

• W1566016654 endingPage "30" @default.
• W1566016654 startingPage "1" @default.
• W1566016654 abstract "A detailed finite element analysis of the right rear lug of the American Airlines Flight 587 - Airbus A300-600R was performed as part of the National Transportation Safety Board s failure investigation of the accident that occurred on November 12, 2001. The loads experienced by the right rear lug are evaluated using global models of the vertical tail, local models near the right rear lug, and a global-local analysis procedure. The right rear lug was analyzed using two modeling approaches. In the first approach, solid-shell type modeling is used, and in the second approach, layered-shell type modeling is used. The solid-shell and the layered-shell modeling approaches were used in progressive failure analyses (PFA) to determine the load, mode, and location of failure in the right rear lug under loading representative of an Airbus certification test conducted in 1985 (the 1985-certification test). Both analyses were in excellent agreement with each other on the predicted failure loads, failure mode, and location of failure. The solid-shell type modeling was then used to analyze both a subcomponent test conducted by Airbus in 2003 (the 2003-subcomponent test) and the accident condition. Excellent agreement was observed between the analyses and the observed failures in both cases. The moment, Mx (moment about the fuselage longitudinal axis), has significant effect on the failure load of the lugs. Higher absolute values of Mx give lower failure loads. The predicted load, mode, and location of the failure of the 1985- certification test, 2003-subcomponent test, and the accident condition are in very good agreement. This agreement suggests that the 1985-certification and 2003-subcomponent tests represent the accident condition accurately. The failure mode of the right rear lug for the 1985-certification test, 2003-subcomponent test, and the accident load case is identified as a cleavage-type failure. For the accident case, the predicted failure load for the right rear lug from the PFA is greater than 1.98 times the limit load of the lugs." @default.
• W1566016654 created "2016-06-24" @default.
• W1566016654 creator A5032050249 @default.
• W1566016654 creator A5034745890 @default.
• W1566016654 creator A5043102051 @default.
• W1566016654 creator A5044927009 @default.
• W1566016654 creator A5074786956 @default.
• W1566016654 date "2006-11-20" @default.
• W1566016654 modified "2023-09-24" @default.
• W1566016654 title "Structural Analysis of the Right Rear Lug of American Airlines Flight 587" @default.
• W1566016654 doi "https://doi.org/10.3970/cmes.2007.022.001" @default.
• W1566016654 hasPublicationYear "2006" @default.
• W1566016654 type Work @default.
• W1566016654 sameAs 1566016654 @default.
• W1566016654 citedByCount "1" @default.
• W1566016654 crossrefType "journal-article" @default.
• W1566016654 hasAuthorship W1566016654A5032050249 @default.
• W1566016654 hasAuthorship W1566016654A5034745890 @default.
• W1566016654 hasAuthorship W1566016654A5043102051 @default.
• W1566016654 hasAuthorship W1566016654A5044927009 @default.
• W1566016654 hasAuthorship W1566016654A5074786956 @default.
• W1566016654 hasConcept C113556839 @default.
• W1566016654 hasConcept C127413603 @default.
• W1566016654 hasConcept C135628077 @default.
• W1566016654 hasConcept C2781052500 @default.
• W1566016654 hasConcept C66283442 @default.
• W1566016654 hasConcept C66938386 @default.
• W1566016654 hasConcept C78519656 @default.
• W1566016654 hasConceptScore W1566016654C113556839 @default.
• W1566016654 hasConceptScore W1566016654C127413603 @default.
• W1566016654 hasConceptScore W1566016654C135628077 @default.
• W1566016654 hasConceptScore W1566016654C2781052500 @default.
• W1566016654 hasConceptScore W1566016654C66283442 @default.
• W1566016654 hasConceptScore W1566016654C66938386 @default.
• W1566016654 hasConceptScore W1566016654C78519656 @default.
• W1566016654 hasIssue "1" @default.
• W1566016654 hasLocation W15660166541 @default.
• W1566016654 hasOpenAccess W1566016654 @default.
• W1566016654 hasPrimaryLocation W15660166541 @default.
• W1566016654 hasRelatedWork W101906648 @default.
• W1566016654 hasRelatedWork W141331799 @default.
• W1566016654 hasRelatedWork W1506535452 @default.
• W1566016654 hasRelatedWork W2057900470 @default.
• W1566016654 hasRelatedWork W2126139822 @default.
• W1566016654 hasRelatedWork W2191858781 @default.
• W1566016654 hasRelatedWork W2208450127 @default.
• W1566016654 hasRelatedWork W2321362139 @default.
• W1566016654 hasRelatedWork W2334313581 @default.
• W1566016654 hasRelatedWork W2598090637 @default.
• W1566016654 hasRelatedWork W2605680329 @default.
• W1566016654 hasRelatedWork W282059290 @default.
• W1566016654 hasRelatedWork W2902409576 @default.
• W1566016654 hasRelatedWork W2961002144 @default.
• W1566016654 hasRelatedWork W3196468744 @default.
• W1566016654 hasRelatedWork W342259241 @default.
• W1566016654 hasRelatedWork W761027710 @default.
• W1566016654 hasRelatedWork W817714089 @default.
• W1566016654 hasRelatedWork W850704692 @default.
• W1566016654 hasRelatedWork W294382523 @default.
• W1566016654 hasVolume "22" @default.
• W1566016654 isParatext "false" @default.
• W1566016654 isRetracted "false" @default.
• W1566016654 magId "1566016654" @default.
• W1566016654 workType "article" @default.