Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads
IR@NAL: CSIR-National Aerospace Laboratories, Bangalore
View Archive Info| Field | Value | |
| Title |
Development of a High Pressure Ratio Axial Fan Stage with Non-metallic Rotor Blads
|
|
| Creator |
Shobhavathy, MT
Prathapanayaka, R Jayaraman, M Dilip Kumar, B Satishkumar, S Samiullah, TH Rajagopal, RS Janaki, Rami Reddy |
|
| Subject |
Aeronautics (General)
Aircraft Propulsion and Power |
|
| Description |
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.
|
|
| Publisher |
NAL
|
|
| Type |
Proj.Doc/Technical Report
NonPeerReviewed |
|
| Identifier |
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.
|
|
| Relation |
http://nal-ir.nal.res.in/8932/
|
|