The influence of fan root flow on the aerodynamic of a low-pressure compressor transition duct

To reduce fuel-burn and emissions there is a drive towards higher bypass ratio and smaller high-pressure ratio core engines. This makes the design of the ducts connecting compressor spools more challenging as the higher radius change increases aerodynamic loading. This is exacerbated at inlet to the...

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Bibliographic Details

Main Authors:	Duncan Walker, Ian Mariah, Dimitra Tsakmakidou, Hiren Vadhvana, Chris Hall
Format:	Default Article
Published:	2019
Subjects:	Aerospace engineering not elsewhere classified Mechanical engineering not elsewhere classified Fan Compressor Gas Turbine InterDuct CFD Aerodynamics Experimental Mechanical Engineering & Transports Aerospace Engineering Mechanical Engineering
Online Access:	https://hdl.handle.net/2134/10048328.v1
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