Wan Norhafizan , Wan Rohizan (2008) Rotorblade Aerodynamic Performance Evaluation. Project Report. UTeM, Melaka, Malaysia. (Submitted)
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Abstract
The goal of this project is to analyse the aerodynamics performance of rotor blade. This analysis involves aerodynamic theory and wind tunnel testing. For wind tunnel analysis, an airfoil model was developed and tested in the wind tunnel with target to assess the performance of rotor blade under almost real conditions. Data collected from the test was compared and validated with the data obtained from various sources, including from industry. The evaluated aspects on this project were coefficient of lift and drag. This project provides understanding on rotor blade performance and the characteristic of NACA 23012 rotor blade profile.
| Item Type: | Final Year Project (Project Report) |
|---|---|
| Uncontrolled Keywords: | Aerodynamics |
| Subjects: | T Technology > T Technology (General) T Technology > TL Motor vehicles. Aeronautics. Astronautics |
| Divisions: | Library > Final Year Project > FKM |
| Depositing User: | Ahmad Abu Bakar |
| Date Deposited: | 08 Mar 2012 07:40 |
| Last Modified: | 28 May 2015 02:22 |
| URI: | http://digitalcollection.utem.edu.my/id/eprint/1263 |
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