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Year of Publication
2014
Journal
International Review of Aerospace Engineering 7 (1), 17-24, 2014
Volume
7
Number of Pages
17-24
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Simulation of a transonic axial flow fan of a high bypass ratio turbofan engine during flight conditions

Assistant Professor of Mechanical Engineering

Citation: 1.Simulation of a transonic axial flow fan of a high bypass ratio turbofan engine during flight conditions. International Review of Aerospace Engineering 7 (1), 17-24, 2014. 2014;7:17-24.

In: International Review of Aerospace Engineering 7 (1), 17-24, 2014

Published by: HZ Hassan, MH Gobran, AA El-Azim , 2014

Cited by: 4