FRINK Linked Data Fragments server

Matches in SemOpenAlex for { <https://semopenalex.org/work/W2086598103> ?p ?o ?g. }

• W2086598103 endingPage "236" @default.
• W2086598103 startingPage "223" @default.
• W2086598103 abstract "The problem of linear flutter analysis in the presence of structural uncertainty is addressed. Whereas the propagation of uncertain structural parameters in finite element models has been carried out by a number of different methods, there appears to be less published work on the influence of random structural parameters on flutter speed. In this paper, we first evaluate the sensitivity of aeroelastic damping to a number of uncertain structural, geometrical and structural-damping parameters. The most significant parameters are identified and then randomised. Secondly, interval, fuzzy and probabilistic methods are used to propagate the structural uncertainty through the aeroelastic analysis resulting in regions of flutter-boundary uncertainty characterised by intervals, fuzzy membership functions and probability density functions. Interval analysis requires two optimisation procedures in order to find the bounds of the aeroelastic responses. The Response Surface Method (RSM) permits efficient optimisation and is used for the estimation of the gradient and Hessian. The resulting intervals are checked using Monte–Carlo Simulation (MCS). Probabilistic analysis is carried out using both first- and second-order perturbation, using the gradient and the Hessian determined by RSM. The first-order perturbation method is generally found to produce results in good agreement with the MCS, although there are differences at the tails of the distributions, especially for the unstable modes close to the flutter speed. The second-order perturbation method provides an improved prediction of the nonlinear behaviour at the tails. The flutter membership function predicted by the fuzzy method generally includes the nonlinear behaviour at the tails of the MCS distribution. Variability in structural mass and stiffness parameters is shown to have a significant effect upon the flutter intervals. Structural damping results in a small but significant increase in the flutter speed, but structural-damping variability does not translate into significant intervals of flutter-boundary uncertainty. Studies are carried out on the Goland wing, with and without structural damping, and on a generic fighter model." @default.
• W2086598103 created "2016-06-24" @default.
• W2086598103 creator A5009550667 @default.
• W2086598103 creator A5022237206 @default.
• W2086598103 creator A5023944664 @default.
• W2086598103 date "2010-02-01" @default.
• W2086598103 modified "2023-10-18" @default.
• W2086598103 title "Propagation of structural uncertainty to linear aeroelastic stability" @default.
• W2086598103 cites W1967526477 @default.
• W2086598103 cites W1970185852 @default.
• W2086598103 cites W1979593580 @default.
• W2086598103 cites W1980160063 @default.
• W2086598103 cites W1991910254 @default.
• W2086598103 cites W1999820269 @default.
• W2086598103 cites W2001695320 @default.
• W2086598103 cites W2008279681 @default.
• W2086598103 cites W2019738352 @default.
• W2086598103 cites W2020591986 @default.
• W2086598103 cites W2035059039 @default.
• W2086598103 cites W2055382966 @default.
• W2086598103 cites W2058042636 @default.
• W2086598103 cites W2065884924 @default.
• W2086598103 cites W2083473180 @default.
• W2086598103 cites W2088024474 @default.
• W2086598103 cites W2098018440 @default.
• W2086598103 cites W2100291155 @default.
• W2086598103 cites W2320570488 @default.
• W2086598103 cites W2322687145 @default.
• W2086598103 doi "https://doi.org/10.1016/j.compstruc.2009.10.005" @default.
• W2086598103 hasPublicationYear "2010" @default.
• W2086598103 type Work @default.
• W2086598103 sameAs 2086598103 @default.
• W2086598103 citedByCount "56" @default.
• W2086598103 countsByYear W20865981032012 @default.
• W2086598103 countsByYear W20865981032013 @default.
• W2086598103 countsByYear W20865981032014 @default.
• W2086598103 countsByYear W20865981032015 @default.
• W2086598103 countsByYear W20865981032016 @default.
• W2086598103 countsByYear W20865981032017 @default.
• W2086598103 countsByYear W20865981032018 @default.
• W2086598103 countsByYear W20865981032019 @default.
• W2086598103 countsByYear W20865981032020 @default.
• W2086598103 countsByYear W20865981032021 @default.
• W2086598103 countsByYear W20865981032022 @default.
• W2086598103 countsByYear W20865981032023 @default.
• W2086598103 crossrefType "journal-article" @default.
• W2086598103 hasAuthorship W2086598103A5009550667 @default.
• W2086598103 hasAuthorship W2086598103A5022237206 @default.
• W2086598103 hasAuthorship W2086598103A5023944664 @default.
• W2086598103 hasConcept C105795698 @default.
• W2086598103 hasConcept C11413529 @default.
• W2086598103 hasConcept C117185709 @default.
• W2086598103 hasConcept C121332964 @default.
• W2086598103 hasConcept C123614077 @default.
• W2086598103 hasConcept C127413603 @default.
• W2086598103 hasConcept C13393347 @default.
• W2086598103 hasConcept C146978453 @default.
• W2086598103 hasConcept C154945302 @default.
• W2086598103 hasConcept C158622935 @default.
• W2086598103 hasConcept C177918212 @default.
• W2086598103 hasConcept C19499675 @default.
• W2086598103 hasConcept C203616005 @default.
• W2086598103 hasConcept C21200559 @default.
• W2086598103 hasConcept C24326235 @default.
• W2086598103 hasConcept C2775924081 @default.
• W2086598103 hasConcept C2777834885 @default.
• W2086598103 hasConcept C28826006 @default.
• W2086598103 hasConcept C32230216 @default.
• W2086598103 hasConcept C33923547 @default.
• W2086598103 hasConcept C41008148 @default.
• W2086598103 hasConcept C47446073 @default.
• W2086598103 hasConcept C49937458 @default.
• W2086598103 hasConcept C62520636 @default.
• W2086598103 hasConceptScore W2086598103C105795698 @default.
• W2086598103 hasConceptScore W2086598103C11413529 @default.
• W2086598103 hasConceptScore W2086598103C117185709 @default.
• W2086598103 hasConceptScore W2086598103C121332964 @default.
• W2086598103 hasConceptScore W2086598103C123614077 @default.
• W2086598103 hasConceptScore W2086598103C127413603 @default.
• W2086598103 hasConceptScore W2086598103C13393347 @default.
• W2086598103 hasConceptScore W2086598103C146978453 @default.
• W2086598103 hasConceptScore W2086598103C154945302 @default.
• W2086598103 hasConceptScore W2086598103C158622935 @default.
• W2086598103 hasConceptScore W2086598103C177918212 @default.
• W2086598103 hasConceptScore W2086598103C19499675 @default.
• W2086598103 hasConceptScore W2086598103C203616005 @default.
• W2086598103 hasConceptScore W2086598103C21200559 @default.
• W2086598103 hasConceptScore W2086598103C24326235 @default.
• W2086598103 hasConceptScore W2086598103C2775924081 @default.
• W2086598103 hasConceptScore W2086598103C2777834885 @default.
• W2086598103 hasConceptScore W2086598103C28826006 @default.
• W2086598103 hasConceptScore W2086598103C32230216 @default.
• W2086598103 hasConceptScore W2086598103C33923547 @default.
• W2086598103 hasConceptScore W2086598103C41008148 @default.
• W2086598103 hasConceptScore W2086598103C47446073 @default.
• W2086598103 hasConceptScore W2086598103C49937458 @default.
• W2086598103 hasConceptScore W2086598103C62520636 @default.
• W2086598103 hasIssue "3-4" @default.

• next