Aerodynamic performance of a coolant flow off-take downstream of an OGV

Within the compression system of a gas turbine engine a significant amount of air is removed to fulfil various requirements associated with cooling, ventilation and sealing. Flow is usually removed through off-takes located in regions where space is restricted, whilst the flow is highly complex cont...

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Bibliographic Details
Main Authors: Chris A'Barrow, Jon Carrotte, Duncan Walker, A.M. Rolt
Format: Default Conference proceeding
Published: 2012
Subjects:
Aerospace engineering not elsewhere classified
Mechanical engineering not elsewhere classified
Other engineering not elsewhere classified
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Aerospace Engineering
Mechanical Engineering
Engineering not elsewhere classified
Online Access:https://hdl.handle.net/2134/19078
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