Hacks, Alexander; Abd El Hussein, Ihab; Ren, Haikun; Schuster, Sebastian; Brillert, Dieter; Abd El Hussein, Ihab:
Experimental Data of Supercritical Carbon Dioxide (sCO₂) Compressor at Various Fluid States
In: Journal of Engineering for Gas Turbines and Power, Jg. 144 (2022), Heft 4, Artikel 041012
2022Artikel/Aufsatz in ZeitschriftOA Hybrid
MaschinenbauFakultät für Ingenieurwissenschaften » Maschinenbau und Verfahrenstechnik » Institut für Energie- und Umweltverfahrenstechnik » Strömungsmaschinen
Damit verbunden: 2 Publikation(en)
Titel in Englisch:
Experimental Data of Supercritical Carbon Dioxide (sCO₂) Compressor at Various Fluid States
Autor*in:
Hacks, AlexanderUDE
GND
1197255834
LSF ID
58288
ORCID
0000-0002-6599-4830ORCID iD
Sonstiges
der Hochschule zugeordnete*r Autor*in
;
Abd El Hussein, IhabUDE
LSF ID
59691
Sonstiges
der Hochschule zugeordnete*r Autor*in
;
Ren, HaikunUDE
GND
1231035501
LSF ID
60676
ORCID
0000-0003-0035-1241ORCID iD
Sonstiges
der Hochschule zugeordnete*r Autor*in
;
Schuster, SebastianUDE
GND
1084245817
LSF ID
52923
ORCID
0000-0002-2055-1163ORCID iD
Sonstiges
der Hochschule zugeordnete*r Autor*in
;
Brillert, DieterUDE
GND
1144405912
LSF ID
55986
ORCID
0000-0002-5025-9163ORCID iD
Sonstiges
der Hochschule zugeordnete*r Autor*in
;
Abd El Hussein, IhabUDE
LSF ID
59691
Sonstiges
der Hochschule zugeordnete*r Autor*in
Erscheinungsjahr:
2022
Open Access?:
OA Hybrid
Web of Science ID
Scopus ID
Sprache des Textes:
Englisch

Abstract in Englisch:

This paper presents experimental data on a centrifugal compressor operated with CO₂. Temperature and pressure at the inlet of the compressor are varied to cover the supercritical region from the liquid-like to the gas-like region. In addition, inlet conditions in the two-phase region are also included. Thus, the experimental test campaign considers thermodynamic conditions relevant for the future energy conversion with sCO₂-Joule cycles. Experimental results are presented as compressor pressure ratio versus inlet mass flow rate at different rotational speeds and throttle positions. Reliable conclusions can be drawn from the experimental results since the reproducibility of the measurements has been demonstrated by conducting experiments in two different test rigs, and measurement uncertainties are reported. The entire compressor geometry is disclosed in a data repository, including computer-aided design models, and input files suitable for mean-line and grid generation programs. Thus, the experimental results are exploitable by the scientific community and pave the road for validated analysis and design tools in the context of the sCO₂-Joule cycle. The presented results open the possibility to estimate uncertainties of analysis and design tools with little effort since geometry information can be quickly integrated. The experimental data are already used in this paper to obtain the accuracy of a computational fluid dynamics (CFD) code and a mean-line program for sCO₂. In addition to quantifying uncertainties, the results presented can be used to identify shortcomings of existing tools. This can be an essential step in the exploration of the sCO₂-Joule cycle.