1
Very high light scattering efficiency. Good flow tracking capability HFSB Helium Filled Soap Bubbles Larger than usual tracing particles Neutrally Buoyant: ≅1 Neutrally Buoyant: ≅1 Introduction Particle image velocimetry (PIV) is an optical measurement technique providing instantaneous velocity vectors in a section of a flow, which allows also turbulent and pressure field analysis. This technique is based on light scattering particles added to the flow, which is illuminated by powerful light source with two pulses separated by short time interval. The scattered light is recorded onto two consecutive frames of a CCD camera. Analysing the displacement of the particles between the two frames is possible to measure the velocity of the flow. Recent developments, like High- speed Tomographic PIV, allow three dimensional, time solved measurements. The characterization of large scale turbulent air flows are of particular interest for industrial applications, in specific the design and optimization of wind turbines, ground vehicles and airplanes . In order to apply 3-D measurements in wide volumes, technical issues must be resolved. Aim of the Project Example of 2-D PIV: Velocity field around an automobile Application of Particle Image Velocimetry in large, industrial wind tunnels Constrains and Problems: PhD Candidate: Giuseppe Caridi Department: AWEP Section: Aerodynamics Supervisor: F. Scarano Promoter: F. Scarano Start date: 1-11-2013 Funding: STW Cooperations: La Vision Type: Scientific Large observation areas Limited power of light source Finite scattering efficiency of tracer particles Limited resolution of the CCD sensors High operational costs of the wind tunnel Possible Solution Aerospace Engineering 2006 Tomographic PIV development 2009 2014 Year Dimension of the field of View A way to study the reliability of the measurement techniques is to analyze simple phenomena. Below is represented the evolution of the measured field of view in the last years on the wake of a cylinder. 160 cm 3 13 cm 3 4000 cm 3 Using HFSB PIV SETUP The development of PIV techniques using HFSB for wind tunnel application involve efforts on two fronts: Technical Theoretical Aerodynamic behaviour of HBSB in different flow regimes. Analysis of tracking capabilities of the HFSB Injection of the Bubbles in the flow Illumination of the region of interest Image-processing The figure shows the comparison of the stream lines generated with the HFSB and the micro size droplets, commonly used in PIV. Methodology

Application of Particle Image...Very high light scattering efficiency. Good flow tracking capability HFSB Helium Filled Soap Bubbles Larger than usual tracing particles Neutrally Buoyant:

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  • Very high light scattering efficiency.

    Good flow tracking capability

    HFSB Helium

    Filled Soap Bubbles

    Larger than usual tracing particles

    Neutrally Buoyant: 𝜌𝐻𝐹𝑆𝐵

    𝜌𝐴𝑖𝑟≅ 1

    Neutrally Buoyant: 𝜌𝐻𝐹𝑆𝐵

    𝜌𝐴𝑖𝑟≅ 1

    Introduction

    Particle image velocimetry (PIV) is an optical measurement technique providing instantaneous velocity vectors in a section of a flow, which allows also turbulent and pressure field analysis.

    This technique is based on light scattering particles added to the flow, which is illuminated by powerful light source with two pulses separated by short time interval. The scattered light is recorded onto two consecutive frames of a CCD camera. Analysing the displacement of the particles between the two frames is possible to measure the velocity of the flow. Recent developments, like High-speed Tomographic PIV, allow three dimensional, time solved measurements.

    The characterization of large scale turbulent air flows are of particular interest for industrial applications, in specific the design and optimization of wind turbines, ground vehicles and airplanes . In order to apply 3-D measurements in wide volumes, technical issues must be resolved.

    Aim of the Project

    Example of 2-D PIV: Velocity field around an automobile

    Application of Particle Image

    Velocimetry in large, industrial

    wind tunnels

    Constrains and Problems:

    PhD Candidate: Giuseppe Caridi Department: AWEP Section: Aerodynamics Supervisor: F. Scarano Promoter: F. Scarano Start date: 1-11-2013 Funding: STW Cooperations: La Vision Type: Scientific

    Large observation areas

    Limited power of light source

    Finite scattering efficiency of tracer particles

    Limited resolution of the CCD sensors

    High operational costs of the wind tunnel

    Possible Solution

    Aero

    space

    Engin

    eering

    2006

    Tomographic PIV development

    2009

    2014

    Year Dimension of the field of View

    A way to study the reliability of the measurement techniques is to analyze simple phenomena. Below is represented the evolution of the measured field of view in the last years on the wake of a cylinder.

    160 cm3

    13 cm3

    4000 cm3

    Using HFSB

    PIV SETUP

    The development of PIV techniques using HFSB for wind tunnel application involve efforts on two fronts:

    Technical Theoretical

    • Aerodynamic behaviour of HBSB in different flow regimes.

    • Analysis of tracking capabilities of the HFSB

    • Injection of the Bubbles in the flow

    • Illumination of the region of interest

    • Image-processing

    The figure shows the comparison of the stream lines generated with the HFSB and the micro size droplets, commonly used in PIV.

    Methodology