NUMERICAL INVESTIGATION OF VORTEXINDUCED VIBRATIONS (VIV) OF A ROTATING CYLINDER IN IN-LINE AND CROSS-FLOW DIRECTIONS SUBJECTED TO OSCILLATORY FLOW / (Record no. 607303)

000 -LEADER
fixed length control field 02493nam a22001697a 4500
003 - CONTROL NUMBER IDENTIFIER
control field NUST
082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER
Classification number 621
100 ## - MAIN ENTRY--PERSONAL NAME
Personal name Ur Rehman, Ubaid
245 ## - TITLE STATEMENT
Title NUMERICAL INVESTIGATION OF VORTEXINDUCED VIBRATIONS (VIV) OF A ROTATING CYLINDER IN IN-LINE AND CROSS-FLOW DIRECTIONS SUBJECTED TO OSCILLATORY FLOW /
Statement of responsibility, etc. Ubaid Ur Rehman
264 ## - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE
Place of production, publication, distribution, manufacture Islamabad :
Name of producer, publisher, distributor, manufacturer SMME- NUST;
Date of production, publication, distribution, manufacture, or copyright notice 2023.
300 ## - PHYSICAL DESCRIPTION
Extent 66p. ;
Other physical details Soft Copy
Dimensions 30cm.
520 ## - SUMMARY, ETC.
Summary, etc. This study aims to explore the phenomenon of Vortex-Induced Vibration (VIV) generated<br/>by cylinder undergoing rotation at different rotation rates (α = 0, 0.25, 0.5, 0.75, and 1) while<br/>being subjected to oscillatory flow in two dimensional numerical simulations. The simulations<br/>use two different Keulegan-Carpenter (KC) numbers KC = 5 and 10, at Reynolds number Re<br/>= 150. A widespread reduced velocities range. This research purpose is to explore the<br/>phenomenon of Vortex-Induced Vibration (VIV) generated by a cylinder undergoing rotation<br/>at different rotation rates ( α = 0, 0.25, 0.5, 0.75, and 1) while being subjected to oscillatory<br/>flow.<br/>The results demonstrate that vibration amplitude in inline and cross-flow directions is<br/>significantly influenced by the rotation provided to cylinder, as well as the KC number and Vr.<br/>However, it is observed that the cross-flow direction vibrations are more profoundly affected<br/>by the rotation. Case of the stationary cylinder (α = 0), the VIV amplitude in cross-flow<br/>direction almost diminishes once the critical value of reduced velocity is surpassed, specifically<br/>Vr = 6 for KC = 5 and Vr = 11 for KC = 10. On other hand, for rotating cylinders (α ≠ 0), the<br/>vibration amplitude reaches zero only at the critical value of reduced velocity. Beyond this<br/>point, it gradually increases and eventually stabilizes.<br/>The critical reduced velocity, which determines the point at which the vibration amplitude<br/>essentially becomes zero, depends on the cylinder's relative motion and is considered the<br/>critical reduced velocity when the effective KC number (KCeff) is very small and same trent<br/>also observed for effective reduced velocity (Vr eff) are small. It should be noted that at<br/>significantly higher reduced velocities, a non-vortex shedding regime occurs, indicating a<br/>distinct flow behavior.
650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM
Topical term or geographic name entry element MS Mechanical Engineering
700 ## - ADDED ENTRY--PERSONAL NAME
Personal name Supervisor : Dr. Adnan Munir
856 ## - ELECTRONIC LOCATION AND ACCESS
Uniform Resource Identifier <a href="http://10.250.8.41:8080/xmlui/handle/123456789/35830">http://10.250.8.41:8080/xmlui/handle/123456789/35830</a>
942 ## - ADDED ENTRY ELEMENTS (KOHA)
Source of classification or shelving scheme
Koha item type Thesis
Holdings
Withdrawn status Permanent Location Current Location Shelving location Date acquired Full call number Barcode Koha item type
  School of Mechanical & Manufacturing Engineering (SMME) School of Mechanical & Manufacturing Engineering (SMME) E-Books 12/11/2023 621 SMME-TH-893 Thesis
© 2023 Central Library, National University of Sciences and Technology. All Rights Reserved.