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A genetic algorithms based optimisation tool for the preliminary design of gas turbine combustors

By J.M. Rogero


SIGLEAvailable from British Library Document Supply Centre- DSC:DXN064178 / BLDSC - British Library Document Supply CentreGBUnited Kingdo

Topics: 21B - Combustion, ignition, 21E - Jet turbine engines, gas turbine engines, 09L - Computer-Aided Design (CAD), TOOLBOX, LINER WALL COOLING FLOW, WING PROFILE OPTIMISATION
Publisher: Cranfield (United Kingdom) : Cranfield University
Year: 2002
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Provided by: OpenGrey Repository
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