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.
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:||Proj.Doc/Technical Report (Project Report)|
|Uncontrolled Keywords:||Transonic Axial Fan;Performance characteristics;Stall margin;Carbon Fiber Composite|
|Subjects:||AERONAUTICS > Aeronautics (General)|
AERONAUTICS > Aircraft Propulsion and Power
|Division/Department:||Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division, Propulsion Division|
|Depositing User:||Mr Nisanth|
|Date Deposited:||10 Aug 2010 13:57|
|Last Modified:||13 Aug 2015 12:58|
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