Please use this identifier to cite or link to this item: https://hdl.handle.net/10356/68693
Full metadata record
DC FieldValueLanguage
dc.contributor.authorHu, Ting-
dc.date.accessioned2016-05-31T01:13:36Z-
dc.date.available2016-05-31T01:13:36Z-
dc.date.issued2016-
dc.identifier.urihttp://hdl.handle.net/10356/68693-
dc.description.abstractGas Turbine is efficient machine for converting fuel into energy at near design point. This project draws the boundary conditions from one known operating point on the operation of an industrial and marine gas turbine LM 2500 to simulate with CFX software. Normal operations see combustion taking place only within the combustor as that is the only point fuel is introduced. A large gas leak (high flow rates) scenario gives rise to the possibility that the flammable gas passes through the filters before the filter doors are shut. In such a plausible scenario, combustion could take place outside the combustor. This project seeks to understand and preliminarily simulate hot surfaces causing combustion within the first stage of the LM 2500 compressor and the conditions that support this. The investigation would be carried out computationally.en_US
dc.format.extent76 p.en_US
dc.language.isoenen_US
dc.rightsNanyang Technological University-
dc.subjectDRNTU::Engineering::Mechanical engineering::Motors, engines and turbinesen_US
dc.titleSimulation of ingestion of flammable gas mixture by a gas turbine compressor in CFXen_US
dc.typeFinal Year Project (FYP)en_US
dc.contributor.supervisorNg Yin Kweeen_US
dc.contributor.schoolSchool of Mechanical and Aerospace Engineeringen_US
dc.description.degreeBachelor of Engineering (Mechanical Engineering)en_US
item.fulltextWith Fulltext-
item.grantfulltextrestricted-
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)
Files in This Item:
File Description SizeFormat 
HuTing FYP report pdf.pdf
  Restricted Access
18.57 MBAdobe PDFView/Open

Page view(s)

183
Updated on Nov 27, 2022

Download(s) 50

20
Updated on Nov 27, 2022

Google ScholarTM

Check

Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.