Fluid-Structure Acoustic Analysis with Bidirectional Coupling and Sound Transmission



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VPE Swiss Workshop Acoustic Simulation 12. Sept. 2013 Fluid-Structure Acoustic Analysis with Bidirectional Coupling and Sound Transmission Reinhard Helfrich INTES GmbH, Stuttgart info@intes.de www.intes.de INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 1

INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 2

Fluid-Structure Acoustics Methods like structural dynamics (vibrations) Application for fluids only (Acoustics) and for structures coupled with fluids (Fluid-Structure Acoustics) Extension of classical structural models by surrounding fluid models using a strong coupling The coupling is performed physically, i.e. the normal displacement of the structure is identical to the normal displacement of the fluid INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 3

Example for Fluid-Structure Acoustics External fluid Structure Doubly wetted shell elements Hull Internal fluid INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 4

Fluid Model with Finite Elements INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 5

Coupling of Structure and Fluid Fluid mesh and structural mesh are usually not compatible. Fluid Incompatible meshes Coupling elements Solid Reasons: Fluid and structure are meshed independently Structural meshes are usually much finer than the coupled fluid mesh due to different sound velocities Incompatible meshes as standard feature are solving the different requirements INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 6

Sound Radiation Anechoic boundaries are modeled by radiation boundary condition elements, e.g. spherical boundaries following Bayliss-Turkel Radiation boundary condition Fluid mesh Structure as sound source INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 7

Surface Waves Surface waves Fluid elements Mode 1 at 0.599 Hz Mode 2 at 0.886 Hz Mode 3 at 0.886 Hz INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 8

Added Mass It is frequently sufficient for structural dynamic analysis to include just the mass of a surrounding or enclosed fluids (like surrounding water of ships or enclosed fluids in a tank). To this end, the fluid mass distribution has to be determined correctly. This can be achieved by modeling the fluid. Even an infinitely expanded surrounding fluid (like for a ship) can be taken into account by semi-infinite elements. INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 9

Eigenvalues and Mode Shapes Displacement Pressure distribution Real coupled eigenmode of a rocket tank INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 10

Energy Distribution in Coupled Eigenmodes Partitioning of energy in fluid and structure for coupled eigenmodes enables the identification of structure-dominant, fluid-dominant, and strongly coupled modes INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 11

Dynamic Condensation There are two available options for dynamic condensation of coupled fluids and structures: Wetted Condensation - Separate calculation of fluid modes and structural modes in different substructures. The external modes are displacement modes and pressure modes. - The final solution step is a coupled vibration analysis. Dry Condensation - In the substructures, a coupled eigenvalue problem is solved, i.e. the fluid part will be isolated. The external modes are coupled modes (without pressure dof). - The final solution step is a structural vibration analysis, because no pressure dof exist any more. - Facilitates the use of acoustic components in larger structural components (but the possibility remains to calculate pressure of the condensed fluid). INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 12

Engine with Attached Parts Specific sound radiation power to indicate structrue-borne sound All pictures by courtesy of Daimler AG Influence of the oil in the oil pan on the structureborne sound of engine block and oil pan INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 13

Dynamic Response Absorption in fluid volume Absorption at surface Normal impedance Assumption: INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 14

Interior Noise of an SUV INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 15

Introduction Structure-borne and air-borne sound excitation for Body-in-White (BIW) and Trimmed Body (TB) Comparison of measurement (performed by Autoneum, Winterthur, Switzerland) and calculation (performed by INTES) dp Body in White Vehicle Body in White (BIW) Interior Fluid dp Trimmed Vehicle Trimmed Body Fluid Trim Transfer Matrix Method Structure INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 16

Structure Model and Fluid-Structure Model DISP DOF: 2 900 367 PRES DOF: 502 696 FS coupling to inner fluid Inner fluid FS with inner fluid Structure model Outer fluid and radiation boundary condition FS with outer fluid FS Model FS coupling to outer fluid INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 17

Measurement Points The measurement points are located as follows: 1) Dash (Left and right) 2) Floor (left and right, front and behind) 3) Tunnel (left, top and right) 4) Wheelhouse (left and right) 5) Four microphones in the interior fluid Accelerometer positions Microphones INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 18

Structure- and Air-borne Excitations Type of calculation: Eigenvalue analysis Modal Frequency Response dp V Excitations (Sine sweep from 5 up to 500 Hz): F[ N ] 1) Structure-borne Q F Gear Box Bridge Rear Axis Subframe Structure Dome Left Q [ mm ] 3 s 2 2) Air-borne Engine Bay Gear Box Rear Muffler Wheelhouse INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 19

Measured Quantities Measured quantities for the correlation: v/f Transfer functions (RMS normal velocity / input force) p/f Transfer functions (RMS microphone SPL / input force) v/q Transfer functions (RMS normal velocity / volume velocity acoustic source) p/q Transfer functions (RMS microphone SPL / volume velocity acoustic source) vrms = 20 log 10 v0 =1000 mm/s = 20 log 10 11 = 2.10 MPa N i = 1 The correlation between simulation and measurement is evaluated using Frequency Response Assurance Criterion (FRAC). FRAC = f max max f f i f i FRF FRF meas 2 meas N i = 1 ( f ) FRF ( f ) f max 2 ( f ) FRF ( f ) i N v i 0 f i v 2 i cal cal i i 2 INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 20 p p RMS 0 ( ) f i FRF α α = meas,cal N p 0 p 2 i

Comparison Structure-Borne Sound BIW Measurement/Simulation Structure excitations v/f Response in frequency domain [Hz] Measurement Simulation FRAC Dash Floor Tunnel Wheelhouse INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 21

Comparison Structure-Borne Sound BIW Measurement/Simulation Structure excitations p/f Response in frequency domain [Hz] Measurement Simulation FRAC Microphones Microphone average INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 22

Comparison Air-Borne Sound BIW Measurement/Simulation Acoustic excitations v/q Response in frequency domain [Hz] Measurement Simulation FRAC Floor Tunnel Wheelhouse INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 23

Comparison Air-Borne Sound BIW Measurement/Simulation Acoustic excitations p/q Response in frequency domain [Hz] Measurement Simulation FRAC Microphones Microphone average INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 24

Trimmed Body (TB) There, 80 trimmed regions were considered Kinematical fluid-structure coupling Fluid-structure trim configuration Trim configuration consist of 80 different regions The physical description of the trim material (and the derived impedance matrices) is directly made for the coupling elements (using a software from Autoneum, Winterthur, Switzerland). INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 25

Comparison Structure-Borne Sound TB Measurement/Simulation Structure excitations v/f Response in frequency domain [Hz] BIW TRIM Simulation FRAC Measurement shifted -30 db Simulation Measurement shifted -30 db Dash Floor Tunnel Wheelhouse INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 26

Comparison Structure-Borne Sound TB Measurement/Simulation Structure excitations p/f Response in frequency domain [Hz] BIW TRIM Simulation Measurement shifted -30 db FRAC Microphones Microphone average INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 27

Comparison Air-Borne Sound TB Measurement/Simulation Acoustic excitations v/q Response in frequency domain [Hz] BIW TRIM Simulation FRAC Measurement shifted -30 db Simulation Measurement shifted -30 db Floor Tunnel Wheelhouse INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 28

Comparison Air-Borne Sound TB Measurement/Simulation Acoustic excitations p/q Response in frequency domain [Hz] BIW TRIM Simulation Measurement shifted -30 db FRAC Microphones Microphone average INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 29

Summary Acoustic analysis as extension of structural dynamics by a bidirectional coupling of pressure and displacement degrees of freedom for all fluids (gas and liquid) Direct and efficient computation of coupled real eigenfrequencies and mode shapes Dynamic condensation to displacement degrees of freedom only ( dry condensation) e.g. for subsequent MBS simulations Modal and direct dynamic response analysis in time and frequency domain Interior and exterior fluids in one model enabling sound transmission analysis INTES GmbH, 2013, Stuttgart, Germany VPW Swiss Workshop Acoustic Simulation 12. Sept. 2013 Seite 30