Application of a Total Pressure Sensor in Supersonic Flow for Shock Wave Analysis Under Low-Pressure Conditions

dc.contributor.authorBílek, Michalcs
dc.contributor.authorMaxa, Jiřícs
dc.contributor.authorŠabacká, Pavlacs
dc.contributor.authorBayer, Robertcs
dc.contributor.authorBinar, Tomášcs
dc.contributor.authorBača, Petrcs
dc.contributor.authorVotava, Jiřícs
dc.contributor.authorTobiáš, Martincs
dc.contributor.authorŽák, Marekcs
dc.coverage.issue20cs
dc.coverage.volume25cs
dc.date.issued2025-10-10cs
dc.description.abstractThis study examines the design and implementation of a sensor developed to measure total pressure in supersonic flow conditions using nitrogen as the working fluid. Using a combination of absolute and differential pressure sensors, the total pressure distribution downstream of a nozzle—where normal shock waves are generated—was characterized across a range of low-pressure regimes. The experimental results were employed to validate and calibrate computational fluid dynamics (CFD) models, particularly within pressure ranges approaching the limits of continuum mechanics. The validated analyses enabled a more detailed examination of shock-wave behavior under near-continuum conditions, with direct relevance to the operational environment of differentially pumped chambers in Environmental Scanning Electron Microscopy (ESEM). Furthermore, an entropy increase across the normal shock wave at low pressures was quantified, attributed to the extended molecular mean free path and local deviations from thermodynamic equilibrium.en
dc.description.abstractThis study examines the design and implementation of a sensor developed to measure total pressure in supersonic flow conditions using nitrogen as the working fluid. Using a combination of absolute and differential pressure sensors, the total pressure distribution downstream of a nozzle—where normal shock waves are generated—was characterized across a range of low-pressure regimes. The experimental results were employed to validate and calibrate computational fluid dynamics (CFD) models, particularly within pressure ranges approaching the limits of continuum mechanics. The validated analyses enabled a more detailed examination of shock-wave behavior under near-continuum conditions, with direct relevance to the operational environment of differentially pumped chambers in Environmental Scanning Electron Microscopy (ESEM). Furthermore, an entropy increase across the normal shock wave at low pressures was quantified, attributed to the extended molecular mean free path and local deviations from thermodynamic equilibrium.en
dc.formattextcs
dc.format.extent1-29cs
dc.format.mimetypeapplication/pdfcs
dc.identifier.citationSENSORS. 2025, vol. 25, issue 20, p. 1-29.en
dc.identifier.doi10.3390/s25206291cs
dc.identifier.issn1424-8220cs
dc.identifier.orcid0009-0001-7613-5804cs
dc.identifier.orcid0000-0002-0640-0406cs
dc.identifier.orcid0000-0003-3908-5120cs
dc.identifier.orcid0000-0002-8528-4430cs
dc.identifier.orcid0000-0003-4426-2857cs
dc.identifier.orcid0000-0001-9793-9767cs
dc.identifier.other199086cs
dc.identifier.researcheridITT-5299-2023cs
dc.identifier.researcheridH-7547-2018cs
dc.identifier.scopus43661524200cs
dc.identifier.scopus57095076700cs
dc.identifier.scopus57194409742cs
dc.identifier.scopus54079251600cs
dc.identifier.scopus7004123643cs
dc.identifier.urihttp://hdl.handle.net/11012/255606
dc.language.isoencs
dc.relation.ispartofSENSORScs
dc.relation.urihttps://www.mdpi.com/1424-8220/25/20/6291cs
dc.rightsCreative Commons Attribution 4.0 Internationalcs
dc.rights.accessopenAccesscs
dc.rights.sherpahttp://www.sherpa.ac.uk/romeo/issn/1424-8220/cs
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/cs
dc.subjectAnsys Fluenten
dc.subjectapertureen
dc.subjectCFDen
dc.subjectdifferentially pumped chamberen
dc.subjectESEMen
dc.subjectlow pressureen
dc.subjectnozzleen
dc.subjectpitot sensorsen
dc.subjectshock waveen
dc.subjectAnsys Fluent
dc.subjectaperture
dc.subjectCFD
dc.subjectdifferentially pumped chamber
dc.subjectESEM
dc.subjectlow pressure
dc.subjectnozzle
dc.subjectpitot sensors
dc.subjectshock wave
dc.titleApplication of a Total Pressure Sensor in Supersonic Flow for Shock Wave Analysis Under Low-Pressure Conditionsen
dc.title.alternativeApplication of a Total Pressure Sensor in Supersonic Flow for Shock Wave Analysis Under Low-Pressure Conditionsen
dc.type.driverarticleen
dc.type.statusPeer-revieweden
dc.type.versionpublishedVersionen
sync.item.dbidVAV-199086en
sync.item.dbtypeVAVen
sync.item.insts2025.11.20 15:49:20en
sync.item.modts2025.11.20 15:20:39en
thesis.grantorVysoké učení technické v Brně. Fakulta elektrotechniky a komunikačních technologií. Ústav elektrotechnologiecs

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