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axial compressor balde optimization

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Old   January 9, 2014, 15:24
Default axial compressor balde optimization
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eslam nagy
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dear all ,
i am studying the effect of the change of blade shape of axial compressor rotor 37 on the efficiency and pressure ratio.

i am using bladegen >>>geometry modeler (blade editor )>turbogride>cfx
and using the design explore as an optimization tool
the problem is how to make input parameter in the blade editor to create a swept , twist , leand blades without change of the blade airfoils

thanks for help
eslam
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