Aerodynamic and Mechanical Design of Compressor Blades Including Static Analysis; ; Essers, Jean-André et alin Proceedings od the 3rd World Congress of Structural and Multidisciplinary Optimization (1999, May) Detailed reference viewed: 66 (4 ULg) Damage Detection Using Model Updating and Identification Techniques; ; Golinval, Jean-Claude et alConference given outside the academic context (1999) Detailed reference viewed: 7 (0 ULg) On-line Damage Assessment Using Operating Deflection Shapes; Golinval, Jean-Claude ; Conference given outside the academic context (1999) Detailed reference viewed: 11 (0 ULg) Finite Element Model Updating Based On Holographic and Speckle Interferometry Measurements: Rapport VIA-25; Golinval, Jean-Claude ![]() Conference given outside the academic context (1999) Optical measurement techniques look very promising for finite element (F.E.) model updating or error localisation of plate-like structures in the field of structural dynamics. The purpose of this paper is ... [more ▼] Optical measurement techniques look very promising for finite element (F.E.) model updating or error localisation of plate-like structures in the field of structural dynamics. The purpose of this paper is to investigate a way to better exploit the high spatial resolution inherent to these techniques in order to correct FE mesh discretisation errors and/or model parameter errors. An important assumption in F.E. model error detection is first to consider the initial mesh as sufficiently fine to well represent the measured (displacement or stress) field. In the case of model updating, the adjustment of the model is performed by minimising the difference between the outputs of the model and the exact solution with respect to design parameters. In the case of FE mesh adaptation, the exact solution has to be estimated whereas in the case of model parameter errors, it is directly measured. The idea developed in this paper is to take advantage of the high spatial resolution offered by optical techniques to calculate successively two error estimators using only measurements. The experimental field is first used for the detection of singular regions corresponding to high gradients. This estimator indicates the regions where a mesh refinement is required. Thus a second estimator is calculated and used for parameter error detection. [less ▲] Detailed reference viewed: 20 (1 ULg) Experimental Validation of Two Nonlinear Identification Techniques on a Single Degree of Freedom System; Golinval, Jean-Claude ; et alConference given outside the academic context (1999) The identification of a single degree of freedom non-linear system is performed on experimental data using two different techniques : a method based on the Wavelet transform and a Direct Parameter ... [more ▼] The identification of a single degree of freedom non-linear system is performed on experimental data using two different techniques : a method based on the Wavelet transform and a Direct Parameter estimation method. Both techniques are based on the analysis of the system free responses and result in the estimation of linear and non-linear physical parameters. The agreement between the two methods was found to be encouraging and opens to the possibility of extending them to the analysis of more complicated systems. [less ▲] Detailed reference viewed: 22 (1 ULg) Punch Press Vibration Isolation: a Case HistoryGolinval, Jean-Claude ; Géradin, Michel ![]() in European Journal of Mechanical and Environmental Engineering (1999), 44(3), 141-145 Detailed reference viewed: 27 (0 ULg) Identification of the Mechanical and Piezoelectric Parameters of a Massively Piezoelectric Structure; ; Golinval, Jean-Claude ![]() Conference given outside the academic context (1998) Detailed reference viewed: 10 (2 ULg) On the Reliability of Error Localization Indicators; Golinval, Jean-Claude ; Conference given outside the academic context (1998) Detailed reference viewed: 10 (1 ULg) Model Updating Using Operating Deflection Shapes; Golinval, Jean-Claude ; Conference given outside the academic context (1998) Detailed reference viewed: 37 (0 ULg) Developpement d'une méthodologie d'optimisation aérodynamique et mécanique d'aubes de compresseurs; ; et al in RFM : Revue Française de Mécanique (1998), 4 Le projet décrit dans cet article a pour but de réaliser le dimensionnement des aubages d'un compresseur axial; pour ce faire, des codes de calcul aérodynamique et mécanique sont intégrés dans un ... [more ▼] Le projet décrit dans cet article a pour but de réaliser le dimensionnement des aubages d'un compresseur axial; pour ce faire, des codes de calcul aérodynamique et mécanique sont intégrés dans un processus d'optimisation globale. Le transfert de données entre les différents modules utilisés est pris en charge par un logiciel gestionnaire de tâches, sur lequel est axée la méthode. Les codes aérodynamiques, basés sur l'approche classique quasi-tridimensionnelle, combinent une simulation d'écoulement dans le plan méridien ainsi qu'une succession d'écoulements en grilles d'aubes. Les codes mécaniques permettent une analyse à la fois statique et dynamique des aubages ; on notera en outre la possibilité de leur adjoindre des calculs d'impact ou de vérification de la durée de vie. Dans son état actuel, le code général permet d'optimiser la masse ou le rendement d'un étage de compression sur la base d'un calcul aérodynamique dans le plan méridien et d'une vérification des marges fréquentielles. [less ▲] Detailed reference viewed: 139 (14 ULg) Updating Industrial Models Under a General Optimization Environnment; Golinval, Jean-Claude ; et alConference given outside the academic context (1998) Detailed reference viewed: 5 (0 ULg) A Frequency Domain Correlation Technique for Model Correlation and Updating; Golinval, Jean-Claude ; Conference given outside the academic context (1997) Detailed reference viewed: 30 (0 ULg) Dynamic Stress and Fatigue Life Prediction Using Modal Testing and Model Correlation; Golinval, Jean-Claude ![]() Conference given outside the academic context (1996) Detailed reference viewed: 11 (0 ULg) Modal Analysis of Plate Structures Using Digital Speckle Pattern Interferometry; ; Golinval, Jean-Claude et alConference given outside the academic context (1995) Detailed reference viewed: 30 (1 ULg) A Dynamic Stiffness-Transfer Matrix Method for Forced Response Analysis of One-Dimensional Structures; Golinval, Jean-Claude ; Géradin, Michel ![]() in Journal of Modal Analysis (1994), (Avril), Detailed reference viewed: 31 (1 ULg) Validation of Structural Computation Codes in Elastoviscoplasticity; ; et al in International Journal for Numerical Methods in Engineering (1990), 29 This paper discusses various procedures for the implementation of viscoplastic constitutive equations in Finite Element Codes. The set of constitutive equations that has been used is described. Several ... [more ▼] This paper discusses various procedures for the implementation of viscoplastic constitutive equations in Finite Element Codes. The set of constitutive equations that has been used is described. Several kinds of implementation, using various numerical techniques, are proposed. Validations of these implementations and comparisons between them are investigated by means of a set of simple but comprehensive examples [less ▲] Detailed reference viewed: 16 (1 ULg) Three dimensional turbine blade analysis in thermo-viscoplasticityGéradin, Michel ; Golinval, Jean-Claude ; in La Recherche Aérospatiale (1989), 5(Septembre-Octobre), 51-57 Detailed reference viewed: 21 (0 ULg) Analyse tridimensionnelle d'une aube de turbine en thermo-viscoplasticitéGéradin, Michel ; Golinval, Jean-Claude ; in La recherche aérospatiale (1989), 5(Septembre-Octobre), 51-57 Detailed reference viewed: 67 (2 ULg) |
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