Gas turbine blades Dimentions and Design of aircraft engine

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MecEng
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Hi

I am working on gas turbine design to investigate fatigue and creep failure and i want to design gas turbine blades for aircraft engine. I need to find out the dimension for CAd design
if anyone help me that what should be the dimension of these blades and how many blades attached to roter disc. i also want to find out speed of these baldes means some calculation is well

cheers
Mac
 
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Chances are no one is going to give you a blade profile. If you're just doing tutorials/testing, then just grab a NACA profile and extrude it up a distance that you think is reasonable. Then, model up a dummy shroud and do a cyclic analysis.