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Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer

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dc.contributor.author Snedden, Glen C
dc.date.accessioned 2007-08-02T09:34:45Z
dc.date.available 2007-08-02T09:34:45Z
dc.date.issued 2003-09
dc.identifier.citation Snedden, GC. 2003. Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer. ISABE 2003, 16th International Symposium on Airbreathing Engines, Cleveland, Ohio, 31 August 2003- 9 September 2003, pp 7 en
dc.identifier.uri http://hdl.handle.net/10204/1062
dc.description.abstract A comprehensive computational fluid dynamics (CFD) model of an actual disc cavity, complete with rotation and conjugate heat transfer, is presented. The model uses a commercially available code with geometrical accuracy including a labyrinth seal, all the physics of a rotating system and conjugate heat transfer. Results presented include: flow patterns, pressure distributions and temperature distributions in both the fluid and metal components, as well as heat transfer. Validation results for the temperature of the 1st rotor disc are also presented en
dc.language.iso en en
dc.subject Heat transfer en
dc.subject CFD models en
dc.subject CFD models en
dc.subject ROTOR discs en
dc.title Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer en
dc.type Conference Presentation en
dc.identifier.apacitation Snedden, G. C. (2003). Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer. http://hdl.handle.net/10204/1062 en_ZA
dc.identifier.chicagocitation Snedden, Glen C. "Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer." (2003): http://hdl.handle.net/10204/1062 en_ZA
dc.identifier.vancouvercitation Snedden GC, Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer; 2003. http://hdl.handle.net/10204/1062 . en_ZA
dc.identifier.ris TY - Conference Presentation AU - Snedden, Glen C AB - A comprehensive computational fluid dynamics (CFD) model of an actual disc cavity, complete with rotation and conjugate heat transfer, is presented. The model uses a commercially available code with geometrical accuracy including a labyrinth seal, all the physics of a rotating system and conjugate heat transfer. Results presented include: flow patterns, pressure distributions and temperature distributions in both the fluid and metal components, as well as heat transfer. Validation results for the temperature of the 1st rotor disc are also presented DA - 2003-09 DB - ResearchSpace DP - CSIR KW - Heat transfer KW - CFD models KW - CFD models KW - ROTOR discs LK - https://researchspace.csir.co.za PY - 2003 T1 - Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer TI - Simplified 3d CFD flow simulation of a turbojet disc cavity with conjugate heat transfer UR - http://hdl.handle.net/10204/1062 ER - en_ZA


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