Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads

Shobhavathy, MT and Prathapanayaka, R and Jayaraman, M and Dilip Kumar, B and Satishkumar, S and Samiullah, TH and Rajagopal, RS and Janaki, Rami Reddy Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads. Project Report. NAL, Bangalore.

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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: 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: 10 Aug 2010 13:57
URI: http://nal-ir.nal.res.in/id/eprint/8932

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