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Welcome to ICSV26!
ST

Stephan Tewes

Airbus Operations GmbH
Interior Noise Integration & Vibration
Hamburg, Germany

My Moderators Sessions

Wednesday, July 10
 

10:30 EDT

CHARACTERIZATION OF THE NOISE SHIELDING EFFECT FOR UAS USING AN IMPULSIVE REFERENCE SOUND SOURCE St-Laurent 6

10:50 EDT

VIRTUAL SHAKER TESTING: FROM CONCEPT TO APPLICATIONS FOR SPACECRAFT STRUCTURES St-Laurent 6

11:10 EDT

FLEXURAL WAVE CONCENTRATION EFFECT IN TAPERED RODS AND WEDGE-LIKE BEAMS WITH POWER-LAW THICKNESS St-Laurent 6

11:30 EDT

SIMULATION ANALYSIS AND DESIGN SUGGESTION OF LARGE-SIZE RADIATION-HEATED THERMAL-ACOUSTIC TRAVELING WAVE TUBE St-Laurent 6

11:50 EDT

ACCELERATING THE UNCERTAINTY PROPAGATION OF STRUCTURAL DYNAMICS SYSTEMS USING A SURROGATE-BASED METHOD St-Laurent 6

13:10 EDT

THE INVESTIGATION OF SOUND FIELD UNIFORMITY FOR MULTISOURCE TRAVELING WAVE TUBE USING FEM ANALYSIS St-Laurent 6

13:30 EDT

NONLINEAR VIBRATION ANALYSIS OF A CONTROL FIN WITH FREEPLAY NONLINEARITY St-Laurent 6

15:50 EDT

NONLINEAR ELECTRO-MAGNETO-AEROELASTIC ENERGY HARVESTER MODELING WITH STALL AERODYNAMICS St-Laurent 6

16:10 EDT

NEW APPROACH TO AERODYNAMIC REDUCTION IN GROUND FLUTTER SIMULATION BASED ON GENERALIZED AERODYNAMICS St-Laurent 6

16:30 EDT

CONSTRUCTION AND APPLICATION OF A NEW ACOUSTIC FACILITY OF CHINA St-Laurent 6

17:10 EDT

FULL-SCALE CABIN NOISE FROM TURBULENT BOUNDARY LAYER EXCITATION, PART 1 : WALL-PRESSURE MEASUREMENT AND ANALYSIS St-Laurent 6

17:30 EDT

FULL-SCALE CABIN NOISE FROM TURBULENT BOUNDARY LAYER EXCITATION, PART 2: VIBRO-ACOUSTIC MODELLING AND TRANSMISSION St-Laurent 6
 
Thursday, July 11
 

09:00 EDT

A PARAMETRIC STUDY ON WALL PRESSURE WAVENUMBER-SPECTRUM MODELS WITH APPLICATION TO AIRCRAFT FUSELAGE VIBRATION PREDICTION St-Laurent 6

09:20 EDT

PREDICTION OF THE SPEECH TRANSMISSION QUALITY IN THE PRESENCE OF BACKGROUND NOISE USING THE RAY TRACING TECHNIQUE St-Laurent 6

09:40 EDT

AIRCRAFT PANEL CURVATURE INTERACTION ON ACOUSTIC INSERTION AND TRANSMISSION LOSS PERFORMANCES St-Laurent 6

10:00 EDT

AIRCRAFT SIDE WALL WITH IMPROVED LOW-FREQUENCY SOUND INSULATION USING A LINING PANEL WITH HELMHOLTZ RESONATORS St-Laurent 6

10:40 EDT

COMPARISON OF THE RECEPTION PLATE METHOD AND THE INVERSE FORCE METHOD FOR ASSESSING THE POWER OF A DUMMY VIBRATORY SOURCE St-Laurent 6

11:00 EDT

USING TRANSFER PATH ANALYSIS METHODS FOR ASSESSING THE VELOCITY RESPONSE ON A PLATE GENERATED BY A DUMMY VIBRATORY SOURCE. St-Laurent 6
 

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