@@ -202,4 +202,48 @@ @article{RubiniApplTherm
202202 selected = { true}
203203}
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205+ @phdthesis {rubini_masters ,
206+ edition = { } ,
207+ number = { } ,
208+ journal = { } ,
209+ bibtex_show = { true} ,
210+ abstract = { This work presents an aerothermal investigation of a novel turbomachine used for light olefin production. The
211+ turbomachine – the Roto-Dynamic Reactor (RDR) – replaces the radiant section of a conventional steam cracking
212+ plant. The design objectives are to efficiently transfer shaft work (provided by an electric motor) to the working
213+ fluid whilst minimising the residence time, hydrocarbon partial pressure, coking and secondary reactions, and
214+ increasing the olefin yield and process temperature. The novel reactor is comprised of a 1.5 stage turbomachine
215+ with the outlet of one stage connected to the inlet of the next through a toroidal-shaped vaneless diffuser space.
216+ This yields a regenerative design. The concept is investigated using the in-house CFD code TBLOCK using a
217+ combination of Reynolds-averaged Navier-Stokes (RANS) and large eddy simulation (LES) strategies. Numerical
218+ investigations show a steady rise in temperature across the reactor with a higher outlet temperature (T = 1350 K)
219+ than typical conventional pyrolytic reactors. The pilot design shows a low residence time of 53 ms for an average
220+ particle and significantly higher viscous shear stresses than conventional furnaces. These two factors solidify
221+ the economic feasibility of the concept. This work validates the regenerative nature of the design, with the flow
222+ progressing as nearly independent streamtubes. Numerical results confirm the design requirement of a temporally
223+ and circumferentially uniform inlet field at the inlet of each regenerative pass of the reactor. Secondary and
224+ tip leakage flow mechanisms are explored to determine the impact on work added to the working fluid. The
225+ high-turning impulsive blading results in very large losses in work coefficient. Shock systems are probed in detail
226+ to understand the process of energy transformation into internal energy, in addition to the shockwave/boundary
227+ layer interaction that promotes strong mixing. This internal mixing within a regenerative pass is required to enable
228+ a regenerative design and prevent secondary reactions. The current design exhibits sufficient internal mixing to
229+ decrease the static pressure, but also to drive chemical reaction and crack long-chain hydrocarbons into shorter
230+ molecular structures. This work introduces guidewalls to mitigate lateral mixing between adjacent regenerative
231+ passes and improve the guiding of the flow in the vaneless diffuser space.} ,
232+ pages = { } ,
233+ publisher = { Master's Thesis, University of Oxford} ,
234+ school = { Master's Thesis, University of Oxford} ,
235+ title = { A Novel Turbomachine for Hydrocarbon Cracking: An Aerothermal Investigation} ,
236+ volume = { Master's Thesis} ,
237+ author = { Rubini, Dylan} ,
238+ abbr = { Master's Thesis} ,
239+ editor = { } ,
240+ year = { 2020} ,
241+ month = { 05} ,
242+ url = { http://dx.doi.org/10.13140/RG.2.2.24319.93609} ,
243+ html = { http://dx.doi.org/10.13140/RG.2.2.24319.93609} ,
244+ doi = { http://dx.doi.org/10.13140/RG.2.2.24319.93609} ,
245+ eprint = { http://dx.doi.org/10.13140/RG.2.2.24319.93609} ,
246+ series = { }
247+ }
248+
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