axial compressor balde optimization -- CFD Online Discussion Forums

January 9, 2014, 14:24	axial compressor balde optimization	#1
eslamnagy New Member eslam nagy Join Date: Oct 2012 Location: egypt Posts: 20 Rep Power: 13	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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