Borhan, Luqman Hakim (2017) The Effect Of Number Of Blades On Turbine Cascade Blade Performance By Using 3D CFD. Project Report. UTeM, Melaka, Malaysia. (Submitted)
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The Effect Of Number Of Blades On Turbine Cascade Blade Performance By Using 3D CFD.pdf - Submitted Version Download (454kB) |
Abstract
Gas turbine engines considered as a huge machine with applications in propulsion and for power electric generation. The main parameter that considered in designing the gas turbine engines are the efficiency of turbine blades performance inside the engine. The NACA 8412 airfoil is used to simulate the blade’s cascade and was obtained from the UIUC Airfoil Coordinates Database as a supercritical airfoil. The airfoil is generated into the SOLIDWORKS with specific geometric of the turbine blade profile. The Fluent was used to simulate the cascade for 3 blades, 5 blades, 7 blades and 9 blades. The result for drag coefficient,
| Item Type: | Final Year Project (Project Report) |
|---|---|
| Uncontrolled Keywords: | Turbines, Turbines - Blades - Design and construction, Turbines - Blades |
| Subjects: | T Technology > T Technology (General) T Technology > TJ Mechanical engineering and machinery |
| Divisions: | Library > Final Year Project > FKM |
| Depositing User: | Mohd Hannif Jamaludin |
| Date Deposited: | 31 Dec 2018 09:27 |
| Last Modified: | 31 Dec 2018 09:27 |
| URI: | http://digitalcollection.utem.edu.my/id/eprint/22604 |
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