Enhanced external aerodynamic performance of a generic combustor using an integrated OGV/prediffuser design technique

In this paper we use experimental measurements to characterize the extent that improved the external aerodynamic performance (reduced total pressure loss, increased flow quality) of a gas-turbine combustion system may be achieved by adopting an integrated OGV/prediffuser technique. Two OGV/prediffus...

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Bibliographic Details
Main Authors: Duncan Walker, Jon Carrotte, Jim McGuirk
Format: Default Article
Published: 2007
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/2134/5880
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