Shobhavathy, MT and Prathapanayaka, R and Jayaraman, M and Dileepkumar B , Alone and Satishkumar, S and Samiullah, TH and Rajagopal, RS and Janaki Rami Reddy, M Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads. Project Report. NAL, Bangalore.
Full text not available from this repository.Abstract
This project proposal is submitted to GATET at GTf :E for funding. The research programme envisages the Development of a high Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blades for Small Gas Turbine Engine". The novelty of the Project is to demonstrate a 2: 1 pressure ratio in single stage fan with tip diameter of 316mm, rotor tip speed of 470 m/s and rotational speed of 28400 rpm.
| Item Type: | Monograph (Project Report) |
|---|---|
| Uncontrolled Keywords: | Transonic Axial Fan;Performance characteristics;Stall margin;Carbon Fiber Composite |
| Subjects: | AERONAUTICS > Aeronautics (General) AERONAUTICS > Aircraft Propulsion and Power |
| Depositing User: | Mr Nisanth |
| Date Deposited: | 10 Aug 2010 08:27 |
| Last Modified: | 13 Aug 2015 07:28 |
| URI: | http://nal-ir.nal.res.in/id/eprint/8932 |
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