Effect of nozzle assembly, insulation and operating condition on partial combustion unit performance : (Record no. 7313)

MARC details
000 -LEADER
fixed length control field 04495ntm a2200277 a 4500
001 - CONTROL NUMBER
control field vtls000101546
003 - CONTROL NUMBER IDENTIFIER
control field KUKTEM
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20251117113346.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 171004t2017 my a f abm 000 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number THE0000936(Local)
039 #9 - LEVEL OF BIBLIOGRAPHIC CONTROL AND CODING DETAIL [OBSOLETE]
Level of rules in bibliographic description 201905271023
Level of effort used to assign nonsubject heading access points nazirah
-- 201710041126
-- nazri
040 ## - CATALOGING SOURCE
Original cataloging agency UMP
090 ## - LOCALLY ASSIGNED LC-TYPE CALL NUMBER (OCLC); LOCAL CALL NUMBER (RLIN)
Classification number (OCLC) (R) ; Classification number, CALL (RLIN) (NR) FKKSA .L39 2017 r Thesis
100 1# - MAIN ENTRY--PERSONAL NAME
Personal name Law, Woon Phui
245 10 - TITLE STATEMENT
Title Effect of nozzle assembly, insulation and operating condition on partial combustion unit performance :
Remainder of title computational fluid dynamics and experimental study /
Statement of responsibility, etc. Law Woon Phui
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Kuantan, Pahang :
Name of publisher, distributor, etc. UMP,
Date of publication, distribution, etc. 2017
300 ## - PHYSICAL DESCRIPTION
Extent xx, 163 p. :
Other physical details ill. (some col.) ;
Dimensions 30 cm. +
Accompanying material 1 CD ROM
500 ## - GENERAL NOTE
General note Faculty of Chemical and Natural Resources Engineering
502 ## - DISSERTATION NOTE
Dissertation note Thesis (Doctor of Philosophy in Chemical Engineering) -- University Malaysia Pahang – 2017
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc. note Bibliography : p. 126-148
520 3# - SUMMARY, ETC.
Summary, etc. Partial combustion of syngas is often used to produce high-quality metallic iron in steel processing plant. Partial combustion unit (PCU) suffers from insufficient high temperature due to improper design configuration and heat loss. Consequently, higher rate of fuel injection and operating cost is required to maintain the quality of iron. Hence, a proper retrofit of design on the PCU is vital to offer better combustion performance and to reduce fuel consumption. This work aims to address the issues by proposing several new nozzle assembly designs and by installing thermal insulator to the existing PCU. Three new nozzle assembly designs were proposed to offer better turbulent mixing, whereas four different thermal insulators (i.e., brick, iron cast, ceramic fibre and graphite felt) were tested to minimize the heat loss. Experimental measurement is not applicable for opaque wall of PCU and hence computational fluid dynamics (CFD) technique is used to study the reactive fluid flow and heat transfer in the PCU. CFD simulation of the PCU at extreme temperatures is challenging owing to the coupling between the turbulence, chemistry and heat transfer. Hence, a CFD simulation must be validated before it can be routinely used. The validation was performed using the LDV measurement of a scale-down PCU rig, as well as by comparing with the published measurements. Three turbulence models, namely standard k-ε (SKE), Reynolds stress model (RSM) and scale-adaptive simulation (SAS) were employed. Combustion reaction was modelled using the eddy dissipation model (EDM) and detailed chemistry flamelet models, whereas the heat transfer was calculated by considering a convection, conduction and radiation. Discrete ordinates (DO) and spherical harmonics (P-1) were used for radiative heat transfer. The inlet of PCU and nozzle is treated as inlet velocity with species mixture while the wall is assumed as non-slip boundary. The finding showed that the non-premixed flame model with detailed chemistry provided a better prediction with 6.58% of deviation from measured temperature. It was found that the prediction without considering radiation yielded over 9% error compared to < 7% error when radiation is modelled. The DO model gave the best prediction of radiative heat transfer with 5.65% of deviation. Besides that, all turbulence models provided a good prediction of outlet temperature with a deviation of less than 6% from measured data. However, SAS gave the best prediction with 5.25% of error. All new nozzle assembly designs achieved over 11% higher temperature where the nozzle with flat surface wing gave the best performance with over 45% increase in temperature than the original wingless PCU. It was found that 40% increase in oxygen flowrate increased the peak temperature by about 12%. Dual-lance was found more effective than the single-lance operating at a similar oxygen flowrate. In addition, installation of insulation enhanced over 17% of peak outlet temperature. The best insulation was achieved using ceramic fibre with 20.4% higher peak temperature than the original non-insulated PCU. The finding from this work may useful for design retrofitting of a PCU, whereby the CFD model can be employed to simulate the PCU performance and the LDV data can be used for validation.
610 20 - SUBJECT ADDED ENTRY--CORPORATE NAME
Corporate name or jurisdiction name as entry element Faculty of Chemical and Natural Resources Engineering
General subdivision Dissertations
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Universities and Colleges
General subdivision Dissertations
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Theses
Holdings
Withdrawn status Lost status Source of classification or shelving scheme Damaged status Not for loan Home library Current library Date acquired Total checkouts Full call number Barcode Date last seen Copy number Price effective from Koha item type
  Not lost Library of Congress Classification   Not for loan UMPLIB GAMBANG UMPLIB GAMBANG 04/09/2019   FKKSA .L39 2017 r Thesis 0000119719 04/09/2019 1 04/09/2019 Thesis
  Not lost Library of Congress Classification   Not for loan UMPLIB GAMBANG UMPLIB GAMBANG 04/09/2019   CD 10825 | FKKSA .L39 2017 r Thesis 0000119720 04/09/2019 1 04/09/2019 Thesis

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