Aerodynamic design of a cooled cooling air system for an aero gas turbine

This paper examines the aerodynamic design requirements of a cooled cooling air system for a large, high by-pass ratio, high overall pressure ratio aero-engine. This can be broken into aerodynamic sub-systems each with their own set of requirements and challenges. A low pressure system is required t...

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Bibliographic Details

Main Authors:	Duncan Walker, Bharat R. Koli, Apostolos Spanelis, Peter Beecroft
Format:	Default Conference proceeding
Published:	2017
Subjects:	Other engineering not elsewhere classified Gas turbine Combustor Cooling Aerodynamics Engineering not elsewhere classified
Online Access:	https://hdl.handle.net/2134/26864
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