Effect of nozzle diameter on jet impingement cooling system / (Record no. 2832)

MARC details
000 -LEADER
fixed length control field 03275nam a2200265 a 4500
001 - CONTROL NUMBER
control field vtls000045655
003 - CONTROL NUMBER IDENTIFIER
control field KUKTEM
005 - DATE AND TIME OF LATEST TRANSACTION
control field 20251114204502.0
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION
fixed length control field 100511t2009 my ao f m 000 0 eng d
020 ## - INTERNATIONAL STANDARD BOOK NUMBER
International Standard Book Number THE0006229(Local)
039 #9 - LEVEL OF BIBLIOGRAPHIC CONTROL AND CODING DETAIL [OBSOLETE]
Level of rules in bibliographic description 201905161120
Level of effort used to assign nonsubject heading access points aida
Level of effort used to assign subject headings 201107132318
Level of effort used to assign classification VLOAD
-- 201005111012
-- ida
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) TJ260 .D85 2009 rs Bc.
100 0# - MAIN ENTRY--PERSONAL NAME
Personal name Dulfharah Nizam Memth Ali
245 10 - TITLE STATEMENT
Title Effect of nozzle diameter on jet impingement cooling system /
Statement of responsibility, etc. Dulfharah Nizam Bin Memth Ali
246 3# - VARYING FORM OF TITLE
Title proper/short title Effect of nozzle diameter on jet impingement cooling system
Medium [electronic resource]
260 ## - PUBLICATION, DISTRIBUTION, ETC.
Place of publication, distribution, etc. Kuantan, Pahang :
Name of publisher, distributor, etc. UMP,
Date of publication, distribution, etc. 2009
300 ## - PHYSICAL DESCRIPTION
Extent xvii, 75 p. :
Other physical details ill. (some col.) ;
Dimensions 30 cm. +
Accompanying material 1 computer disc
502 ## - DISSERTATION NOTE
Dissertation note Project paper (Bachelor of Mechanical Engineering) -- Universiti Malaysia Pahang - 2009
504 ## - BIBLIOGRAPHY, ETC. NOTE
Bibliography, etc. note Bibliography : p. 59-60
520 3# - SUMMARY, ETC.
Summary, etc. This research focused on the study about the effect of nozzle diameter on jet impingement cooling system. The impinging jet can be described as a phenomenon in which the fluid exiting from a nozzle or orifice hits a wall or solid surface usually at normal angle. Impinging air jets have been widely used in many industrial applications in order to achieve enhanced coefficients for convective heating, cooling or drying. A single air jet or arrays of air jets, impinging normally on a surface are an effective method to enhance heat and mass transfer. Engineering applications that widely use air jets include cooling of hot steel plates, tempering of glass plates, drying of textiles and paper, cooling of turbine blades, electronic components and de-icing of aircraft. Experiments were conducted to determine the effect of nozzle diameter on the heat transfer coefficients from a small heat source to a jet impingement cooling system, submerged and confined air. The experiment were carried out with a single jet with three different nozzle diameter, d; 0.5, 1.0, 2.0 cm and four dimensionless jet to heat source spacing, S/d (6, 8, 10, 12) were tested within the laminar jet Reynolds number ranging from 500-2300. The results indicate that the heat transfer coefficient, h increase with the increasing nozzle diameter at the stagnation point region corresponding to 0< r/d <4. This may be attributed to an increase in the jet momentum and turbulence intensity level with the larger nozzle diameter, which results in the heat transfer augmentation. However, the effect of the nozzle diameter on the Nusselt numbers does not exist at the wall jet region corresponding to r/d>4. This may be attributed to the fact that the impinging jet flow characteristics are almost lost in the process of the re-development of the boundary layer after the jet impinges on the plate. By the increasing of the heat transfer coefficient, h the local Nusselt number, Nu also will be increase. This research are significant to improve the overheat component and devices problem nowadays. The results can also significantly increase the performance of the needed component in order to improve product reliability and customer satisfactions.
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Heat
General subdivision Transmission
650 #0 - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element Nozzles
Holdings
Withdrawn status Lost status 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   Not for loan UMPLIB PEKAN UMPLIB PEKAN 04/09/2019   TJ260 .D85 2009 rs Bc. 0000044273 04/09/2019 1 04/09/2019 Final Year Report
  Not lost   Not for loan UMPLIB PEKAN UMPLIB PEKAN 04/09/2019   CD 4160 | TJ260 .D85 2009 rs Bc. 0000044274 04/09/2019 1 04/09/2019 Final Year Report

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