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1 Formulations variationnelles et modèles réduits pour les vibrations de structures contenant des fluides compressibles en l’absence de gravité Cours de Roger Ohayon référence de base Morand-Ohayon /Fluid Structure Interaction / Wiley 1995 Conservatoire National des Arts et Métiers (CNAM) Chaire de Mécanique Laboratoire de Mécanique des structures et des systèmes couplés (www.cnam.fr/lmssc)ohayon@cnam.frohayon@cnam.fr GDR IFS/jeudi 26 juin 2008/14h - 16h
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2 Some local references H. Morand, R. Ohayon / Fluid Structure Interaction/ Wiley – 1995 (chap. 1, 2, 7, 8, 9) R. Ohayon, C. Soize / Structural Acoustic and Vibrations,Academic Press, 1998 R. Ohayon / Fluid Structure Interaction problems / Encyclopedia of Computational Mechanics, vol. 2, Chap. 21, Wiley, 2004
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3 Vibrations of elastic structures
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10 FREQUENCY DOMAIN Measured Transfer Function
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20 REDUCED ORDER MODEL
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23 Non-homogeneous heavy compressible fluid Plane irrotationality
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26 STRUCTURAL ACOUSTIC VIBRATIONS
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37 STRUCTURAL ACOUSTICS EQUATIONS Structure submitted to a fluid pressure loading
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38 Structure submitted to a fluid pressure loading Mechanical elastic stiffness contribution Geometric stiffness contribution Rotation of the normal contribution
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51 REDUCED ORDER MODEL Dynamic substructuring decomposition (Craig-Bampton-Hurty) Fixed/free eigenmodes Static interface deformations
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52 Fluid submitted to a wall normal displacement Linearized Euler equation Constitutive equation Kinematic boundary condition For, we impose in on in
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53 Static pressure field and normal wall displacement relation This case corresponds to a zero frequency situation in which denotes the measure of the volume occupied by domain
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54 Local fluid equations in terms of pressure and wall normal displacement with the constraint in on Helmholtz equation Kinematic boundary condition
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55 Introduction of the displacement potential field with the uniqueness condition
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56 Local fluid equations in terms of displacement potential field and wall normal displacement on in with the uniqueness condition
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57 Pressure-Displacement Unsymmetric Variational Formulation with the constraint
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58 Reduced Order Model First basic problem Acoustic modes in a rigid motionless cavity Orthogonality conditions:
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59 Reduced Order Matrix Model Second basic problem The static pressure solution
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60 Symmetric Matrix Reduced Order Model Decomposition of the admissible space into a direct sum of admissible subspaces: Solution searched under the following form: p and u.n satisfy the constraint
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61 Symmetric Matrix Reduced Order Model where represents a “pneumatic” operator (quasistatic effect of the internal compressible fluid)
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62 Symmetric Matrix Reduced Order Model Hybrid FE/generalized coordinates representation with
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63 Symmetric Matrix Reduced Order Model Generalized coordinates representation
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64 HEAVY / LIGHT COMPRESSIBLE FLUID Gas or Liquid (with/without free surface) The SYMMETRIC reduced order matrix models should be employed with great care: For a light fluid, structural in-vacuo modes can be used For a heavy fluid – liquid, structural in-vacuo modes lead to poor convergence and MANDATORY, added-mass effects must be introduced (this now classical aspect can be introduced via a quasi-static so-called correction or, which is exactly the same, via an added mass operator provided the starting variational formulation contains a proper basic static behavior)
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65 COMPUTATION-EXPERIMENT COMPARISON
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66 Kelvin-Voigt model Thin interface dissipative constitutive equation Structural-acoustic problem with interface damping Particular linear viscoelastic constitutive equation (cf Ohayon-Soize, Structural Acoustics and Vibrations, Academic Press, 1998)
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67 absorbing material Interface wall damping equation Interface wall damping impedance effects
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68 Boundary value problem in terms of (u, p, ) Symmetric formulation of the spectral structural-acoustic problem
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69 CONCLUSION – OPEN PROBLEMS http://www.cnam.fr/lmssc Appropriate Reduced Order Models for Broadband Frequency Domains Hybrid Passive / Active Treatments for Vibrations and Noise Reduction Nonlinearities (Vibrations / Transient Impacts and Shocks)
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