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An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor

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dc.contributor.author Meyers, Bronwyn C
dc.contributor.author Grobler, Jan-Hendrik
dc.contributor.author Snedden, GC
dc.date.accessioned 2023-12-08T09:38:21Z
dc.date.available 2023-12-08T09:38:21Z
dc.date.issued 2023-07
dc.identifier.citation Meyers, B.C., Grobler, J.H. & Snedden, G. 2023. An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor. http://hdl.handle.net/10204/13375 . en_ZA
dc.identifier.uri http://hdl.handle.net/10204/13375
dc.description.abstract A combustor was designed for a 200N micro-gas turbine [1, 2] using the NREC preliminary combustor design method [1, 2, 3]. During the design process, there are various aspects where there are no definitive methodologies for specifying the design detail, such as the design of the hole-sets, and multiple options can be derived that can satisfy the required mass flow split and pressure drop for a particular hole-set. en_US
dc.format Fulltext en_US
dc.language.iso en en_US
dc.relation.uri https://www.aessa.org.za/conference/ en_US
dc.relation.uri https://www.aessa.org.za/wp-content/uploads/2023/07/AeSSA-Annual-Conference-2023-Programme.pdf en_US
dc.source 2023 The Aeronautical Society of South Africa's Annual Conference, ICC, Pretoria, South Africa, 27 – 28 July 2023 en_US
dc.subject Combustor en_US
dc.subject Computational Fluid Dynamics en_US
dc.subject Inlet Swirl en_US
dc.title An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor en_US
dc.type Conference Presentation en_US
dc.description.pages 5 en_US
dc.description.note Paper presented at the 2023 The Aeronautical Society of South Africa's Annual Conference, ICC, Pretoria, South Africa, 27 – 28 July 2023 en_US
dc.description.cluster Defence and Security en_US
dc.description.cluster Smart Places en_US
dc.description.impactarea Aeronautic Systems en_US
dc.description.impactarea Energy Supply and Demand en_US
dc.identifier.apacitation Meyers, B. C., Grobler, J. H., & Snedden, G. (2023). An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor. http://hdl.handle.net/10204/13375 en_ZA
dc.identifier.chicagocitation Meyers, Bronwyn C, Jan H Grobler, and GC Snedden. "An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor." <i>2023 The Aeronautical Society of South Africa's Annual Conference, ICC, Pretoria, South Africa, 27 – 28 July 2023</i> (2023): http://hdl.handle.net/10204/13375 en_ZA
dc.identifier.vancouvercitation Meyers BC, Grobler JH, Snedden G, An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor; 2023. http://hdl.handle.net/10204/13375 . en_ZA
dc.identifier.ris TY - Conference Presentation AU - Meyers, Bronwyn C AU - Grobler, Jan H AU - Snedden, GC AB - A combustor was designed for a 200N micro-gas turbine [1, 2] using the NREC preliminary combustor design method [1, 2, 3]. During the design process, there are various aspects where there are no definitive methodologies for specifying the design detail, such as the design of the hole-sets, and multiple options can be derived that can satisfy the required mass flow split and pressure drop for a particular hole-set. DA - 2023-07 DB - ResearchSpace DP - CSIR J1 - 2023 The Aeronautical Society of South Africa's Annual Conference, ICC, Pretoria, South Africa, 27 – 28 July 2023 KW - Combustor KW - Computational Fluid Dynamics KW - Inlet Swirl LK - https://researchspace.csir.co.za PY - 2023 T1 - An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor TI - An aerodynamic CFD analysis of inlet swirl in a micro-gas turbine combustor UR - http://hdl.handle.net/10204/13375 ER - en_ZA
dc.identifier.worklist 27281 en_US


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