Volume 1A, Symposia: Turbomachinery Flow Simulation and Optimization; Applications in CFD; Bio-Inspired and Bio-Medical Fluid M 2016
DOI: 10.1115/fedsm2016-7506
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Finite Element Approximation of the Extended Fluid-Structure Interaction (eXFSI) Problem

Abstract: This contribution is the second part of three papers on Adaptive Multigrid Methods for the eXtended Fluid-Structure Interaction (eXFSI) Problem, where we introduce a monolithic variational formulation and solution techniques. To the best of our knowledge, such a model is new in the literature. This model is used to design an on-line structural health monitoring (SHM) system in order to determine the coupled acoustic and elastic wave propagation in moving domains and optimum locations for SHM sensors. In a mono… Show more

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Cited by 5 publications
(5 citation statements)
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“…The detailed analysis of the increment of C L max and stall angle is presented in the following table: From the Table-2, it is clear that for NACA 0021 aerofoil the computational gain is higher than the experimental gain for all the velocity ratios, except for case of the zero velocity ratio. Noteworthy, the numerical study does not include the effect of fluid-structure interaction (FSI) [41][42][43][44][45][46][47][48][49][50][51]. Thereby, the associated vibration is neglected in the numerical results.…”
Section: Resultsmentioning
confidence: 99%
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“…The detailed analysis of the increment of C L max and stall angle is presented in the following table: From the Table-2, it is clear that for NACA 0021 aerofoil the computational gain is higher than the experimental gain for all the velocity ratios, except for case of the zero velocity ratio. Noteworthy, the numerical study does not include the effect of fluid-structure interaction (FSI) [41][42][43][44][45][46][47][48][49][50][51]. Thereby, the associated vibration is neglected in the numerical results.…”
Section: Resultsmentioning
confidence: 99%
“…This preliminary study indicates the feasibility of practical implementation of leading edge cylinders for thick aerofoil in aviation, wind turbine, and other applications. The use of the above-mentioned modifications to the aerofoil would add further layer of complexity for the structural health monitoring (SHM) system due to the addition of cylinder-driven vibrations [41][42][43][44][45][46][47][48][49][50][51].…”
Section: Discussionmentioning
confidence: 99%
“…For the damage/delamination studies, to identify skin/stiffener debonding and de- While extensive SHM advancement has been accomplished, a great deal of work is still needed for more practical applications of SHM in composite materials [111]. Through a down-select procedure based on the control and health monitoring of structural design for the space vehicle, the tested SHM sensors and their sensing techniques were chosen [112]. To design online SHM systems for aerospace vehicles or aircraft, an extended fluid-structure interaction was proposed.…”
Section: Aerospace Structuresmentioning
confidence: 99%
“…To design online SHM systems for aerospace vehicles or aircraft, an extended fluid-structure interaction was proposed. It is a strongly coupled version of a standard FSI problem with a wave propagation problem coupled, in which the wave propagation prob-lem is posed on the moving mesh which is automatically adopted from the FSI problem at each time stage [112].…”
Section: Aerospace Structuresmentioning
confidence: 99%
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