DC Field | Value | Language |
---|---|---|
dc.contributor.author | Brueggemann, Christoph | - |
dc.contributor.author | Badum, Lukas | - |
dc.contributor.author | Bauer, Maximilian | - |
dc.contributor.author | Schatz, Markus | - |
dc.contributor.author | Vogt, Damian | - |
dc.date.accessioned | 2020-12-10T07:13:49Z | - |
dc.date.available | 2020-12-10T07:13:49Z | - |
dc.date.issued | 2020 | - |
dc.identifier.issn | 1882-5079 | - |
dc.description.abstract | Pneumatic probes are commonly used to determine the flow vector as well as the thermodynamic state of the fluid in turbomachinery applications. The conventional method to measure a flow passage velocity or pressure field is to move the probe to discrete positions and to hold a certain settling time before valid data can be recorded. This study presents a measurement methodology leading to a reduction in the required measurement duration of up to 70-90%, depending on the level of flow field resolution. The approach is based on the concept of continuously traversing probes as introduced by Gomes et al. [1]. However, the system model is changed by reducing the transfer function to a single PT1-behavior. While the experiments conducted by Gomes et al. [1] were limited to only linear cascade measurements, the method used here is extended to turbomachinery applications with highly complex flow structures. The continuous traverse measurements are validated through a comparison with conventional discrete measurements that include characteristic settling time. For this purpose, tests have been performed in an axial diffuser test rig operated with air and a low pressure steam turbine. The results obtained with the new approach show a good match, thus proving the viability of the proposed method for turbomachinery applications. For future tests, a significant reduction in measurement time and cost can be achieved. | - |
dc.description.sponsorship | Strömungsmaschinen in der Energietechnik | - |
dc.language.iso | eng | - |
dc.publisher | Gas Turbine Society of Japan | - |
dc.relation.ispartof | International Journal of Gas Turbine, Propulsion and Power Systems | - |
dc.title | Fast Traveling Pneumatic Probes for Turbomachinery Applications | - |
dc.type | Working Paper | - |
dc.identifier.doi | 10.38036/jgpp.11.2_9 | - |
dcterms.bibliographicCitation.volume | 11 | - |
dcterms.bibliographicCitation.issue | 2 | - |
dcterms.bibliographicCitation.pagestart | 9 | - |
dcterms.bibliographicCitation.pageend | 16 | - |
dcterms.bibliographicCitation.originalpublisherplace | Tokyo | - |
local.submission.type | only-metadata | - |
item.grantfulltext | none | - |
item.openairetype | Working Paper | - |
item.languageiso639-1 | en | - |
item.fulltext_s | No Fulltext | - |
item.fulltext | No Fulltext | - |
crisitem.author.dept | Strömungsmaschinen in der Energietechnik | - |
crisitem.author.parentorg | Fakultät für Maschinenbau und Bauingenieurwesen | - |
Appears in Collections: | 6 - Publication references (without fulltext) of your publications before HSU |
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