http://www.cnr.it/ontology/cnr/individuo/prodotto/ID194152
Compressor Fouling Modelling: Relationship Between Computational Roughness And Gas Turbine Operation Time (Articolo in rivista)
- Type
- Label
- Compressor Fouling Modelling: Relationship Between Computational Roughness And Gas Turbine Operation Time (Articolo in rivista) (literal)
- Anno
- 2012-01-01T00:00:00+01:00 (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#doi
- 10.1115/1.4004739 (literal)
- Alternative label
Melino, F., Morini, M., Pinelli, M., Peretto, A., Spina P.R. (2012)
Compressor Fouling Modelling: Relationship Between Computational Roughness And Gas Turbine Operation Time
in Journal of engineering for gas turbines and power; ASME-American Society Of Mechanical Engineers, New York (Stati Uniti d'America)
(literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#autori
- Melino, F., Morini, M., Pinelli, M., Peretto, A., Spina P.R. (literal)
- Pagina inizio
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#numeroVolume
- Rivista
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#pagineTotali
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- Note
- ISI Web of Science (WOS) (literal)
- Http://www.cnr.it/ontology/cnr/pubblicazioni.owl#affiliazioni
- CNR, IMEM, I-43100 Parma, Italy; Univ Ferrara, MechLav, I-44100 Ferrara, Italy; Univ Bologna, DIEM, Bologna, Italy; Univ Ferrara, Dipartimento Ingn, I-44100 Ferrara, Italy (literal)
- Titolo
- Compressor Fouling Modelling: Relationship Between Computational Roughness And Gas Turbine Operation Time (literal)
- Abstract
- Gas turbine axial compressor performance is heavily influenced by blade fouling. As a
result, the gas turbines efficiency and producible power output decrease. Performance
degradation of an axial compressor stage due to fouling can be analyzed by means of
simulation through computational fluid dynamics (CFD) codes. Usually these methods
reproduce the deteriorated blades by increasing their surface roughness and thickness.
Another approach is the scaling of compressor stage performance maps. A model based
on stage-by-stage techniques was presented in a previous work. This model is able to estimate
the modifications of the overall compressor performance map as a function of the
operating hours. The aim of the present study is to combine these two different
approaches in order to relate the increase of blade computational surface roughness with
compressor operating hours (literal)
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