Sloshing dynamics investigation by means of non-intrusive measurement techniques

The motion of the free liquid surface inside a reservoir is called sloshing. Itis of large interest in different industrial fields such as satellite and spacecrafttrajectory control, automotive industry, nuclear engineering, buildingdesign, etc. The framework of propellant management on spacecraft i...

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Main Author: Simonini, Alessia
Other Authors: Colinet, Pierre
Format: Doctoral Thesis
Language:en
Published: Universite Libre de Bruxelles 2018
Subjects:
Online Access:https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/3/MAIN.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/4/TableOfContent.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/5/contratAS.pdf
http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/276889
id ndltd-ulb.ac.be-oai-dipot.ulb.ac.be-2013-276889
record_format oai_dc
collection NDLTD
language en
format Doctoral Thesis
sources NDLTD
topic Sciences de l'ingénieur
Sloshing
Optical Measurement Techniques
spellingShingle Sciences de l'ingénieur
Sloshing
Optical Measurement Techniques
Simonini, Alessia
Sloshing dynamics investigation by means of non-intrusive measurement techniques
description The motion of the free liquid surface inside a reservoir is called sloshing. Itis of large interest in different industrial fields such as satellite and spacecrafttrajectory control, automotive industry, nuclear engineering, buildingdesign, etc. The framework of propellant management on spacecraft is ofmain interest for this PhD thesis, even if its outcome can be applied to manyother fields concerned by sloshing.Being able to understand the behavior of the fluid in a reservoir subjectedto extreme environmental conditions means being able to predict its positionand topology inside the tank, for a given external and gravitationalacceleration and a determined thermodynamic condition. The predictionand control of this motion is far from being understood due to the differentparameters that play a role in the dynamic system such as the geometryof the container, the type of external excitation (shape, frequency contentand amplitude), the level of the liquid and finally the kind of liquid. In particular,the design of propulsion systems are affected by this phenomenon,still hampered by the unavailability of validated CFD models. Moreover theexisting experimental studies are mainly based on intrusive and local singlepoint measurement techniques, which give no information on the behaviorof the 3D liquid interface and on the velocity field inside the liquid phase.The main goal of this project has been to extend the experimental approachof liquid sloshing investigation in space propulsion, studying, developing andimproving non-intrusive measurement techniques for free surface behaviorand velocity characterization in the liquid phase. In particular, the free surfacebehavior have been studied by means of Laser Detection and Recordingtechnique (LeDaR), retrieving the profile of the interface over a line, andReference Image Topography technique (RIT), capturing the instantaneous3D interface shape. In addition, Particle Image Velocimetry (PIV) have beenused to measure the 2D velocity field in the main section of the reservoir.Tests performed with water were used as simpler test case to perform thetechniques while liquid nitrogen has been used as replacement uid havingphysical properties similar to real space propellants.The experimental problems of the selected measurement techniques relatedto the particular application have been addressed and a solution has beenproposed. Especially, the selection of tracers which could comply with theuse of a cryogenic fluid while for RIT the possibility to deal with circulardomains and to measure the absolute value of the liquid level. Finally, PIV in wavy ows needed to deal with dynamic curved interfaces for whicha widely-accepted processing algorithm was not available in literature andbesides, the choice of the particles and their seeding procedure in cryogenicsfluids had to be solved.Some applications are shown, which present the potentiality of the techniquesfor a new insight on sloshing flows with the future purpose of providingan accurate database for the verification and validation of numericalsimulations and a better understanding of the phenomena. === Doctorat en Sciences de l'ingénieur et technologie === info:eu-repo/semantics/nonPublished
author2 Colinet, Pierre
author_facet Colinet, Pierre
Simonini, Alessia
author Simonini, Alessia
author_sort Simonini, Alessia
title Sloshing dynamics investigation by means of non-intrusive measurement techniques
title_short Sloshing dynamics investigation by means of non-intrusive measurement techniques
title_full Sloshing dynamics investigation by means of non-intrusive measurement techniques
title_fullStr Sloshing dynamics investigation by means of non-intrusive measurement techniques
title_full_unstemmed Sloshing dynamics investigation by means of non-intrusive measurement techniques
title_sort sloshing dynamics investigation by means of non-intrusive measurement techniques
publisher Universite Libre de Bruxelles
publishDate 2018
url https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/3/MAIN.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/4/TableOfContent.pdf
https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/5/contratAS.pdf
http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/276889
work_keys_str_mv AT simoninialessia sloshingdynamicsinvestigationbymeansofnonintrusivemeasurementtechniques
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spelling ndltd-ulb.ac.be-oai-dipot.ulb.ac.be-2013-2768892019-01-18T17:16:52Z info:eu-repo/semantics/doctoralThesis info:ulb-repo/semantics/doctoralThesis info:ulb-repo/semantics/openurl/vlink-dissertation Sloshing dynamics investigation by means of non-intrusive measurement techniques Simonini, Alessia Colinet, Pierre Vetrano, Maria Rosaria Degrez, Gérard Scheid, Benoît Buchlin, Jean-Marie Theunissen, Raf R. T. Universite Libre de Bruxelles Université libre de Bruxelles, Ecole polytechnique de Bruxelles – Physicien, Bruxelles 2018-09-14 en The motion of the free liquid surface inside a reservoir is called sloshing. Itis of large interest in different industrial fields such as satellite and spacecrafttrajectory control, automotive industry, nuclear engineering, buildingdesign, etc. The framework of propellant management on spacecraft is ofmain interest for this PhD thesis, even if its outcome can be applied to manyother fields concerned by sloshing.Being able to understand the behavior of the fluid in a reservoir subjectedto extreme environmental conditions means being able to predict its positionand topology inside the tank, for a given external and gravitationalacceleration and a determined thermodynamic condition. The predictionand control of this motion is far from being understood due to the differentparameters that play a role in the dynamic system such as the geometryof the container, the type of external excitation (shape, frequency contentand amplitude), the level of the liquid and finally the kind of liquid. In particular,the design of propulsion systems are affected by this phenomenon,still hampered by the unavailability of validated CFD models. Moreover theexisting experimental studies are mainly based on intrusive and local singlepoint measurement techniques, which give no information on the behaviorof the 3D liquid interface and on the velocity field inside the liquid phase.The main goal of this project has been to extend the experimental approachof liquid sloshing investigation in space propulsion, studying, developing andimproving non-intrusive measurement techniques for free surface behaviorand velocity characterization in the liquid phase. In particular, the free surfacebehavior have been studied by means of Laser Detection and Recordingtechnique (LeDaR), retrieving the profile of the interface over a line, andReference Image Topography technique (RIT), capturing the instantaneous3D interface shape. In addition, Particle Image Velocimetry (PIV) have beenused to measure the 2D velocity field in the main section of the reservoir.Tests performed with water were used as simpler test case to perform thetechniques while liquid nitrogen has been used as replacement uid havingphysical properties similar to real space propellants.The experimental problems of the selected measurement techniques relatedto the particular application have been addressed and a solution has beenproposed. Especially, the selection of tracers which could comply with theuse of a cryogenic fluid while for RIT the possibility to deal with circulardomains and to measure the absolute value of the liquid level. Finally, PIV in wavy ows needed to deal with dynamic curved interfaces for whicha widely-accepted processing algorithm was not available in literature andbesides, the choice of the particles and their seeding procedure in cryogenicsfluids had to be solved.Some applications are shown, which present the potentiality of the techniquesfor a new insight on sloshing flows with the future purpose of providingan accurate database for the verification and validation of numericalsimulations and a better understanding of the phenomena. Sciences de l'ingénieur Sloshing Optical Measurement Techniques Doctorat en Sciences de l'ingénieur et technologie info:eu-repo/semantics/nonPublished https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/3/MAIN.pdf https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/4/TableOfContent.pdf https://dipot.ulb.ac.be/dspace/bitstream/2013/276889/5/contratAS.pdf http://hdl.handle.net/2013/ULB-DIPOT:oai:dipot.ulb.ac.be:2013/276889 3 full-text file(s): application/pdf | application/pdf | application/pdf 3 full-text file(s): info:eu-repo/semantics/restrictedAccess | info:eu-repo/semantics/openAccess | info:eu-repo/semantics/closedAccess