A novel approach for the design of axial flow fan by increasing by-pass ratio in a constant-diameter turbofan

The present study introduces an innovative aerodynamic redesign of an axial flow fan based on constant diffusion factor and radial equilibrium. All input design parameters such as mass flow rate, hub to tip ratio, aspect ratio, tip diameter and angular velocity are taken from NASA Rotor 67 as a conv...

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Bibliographic Details
Main Authors: Ali Shahsavari, Mahdi Nili-Ahmadabadi
Format: Article
Language:English
Published: KeAi Communications Co., Ltd. 2020-06-01
Series:Propulsion and Power Research
Subjects:
Online Access:http://www.sciencedirect.com/science/article/pii/S2212540X20300237