have you estimated the stage compression ratio? At such a small scale the blade airfoil matters less due to the Reynolds number. what is the compression ratio that you are shooting for when you have the stages done?
Hello Guys - here is my first attempt on an axial compressor for jet enginge purposes. to go easier with the free form surface design I wrote an automatism in Cad Scripting under Rhino VBR
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Why reach for speed, when you could have precision instead!!!
have you estimated the stage compression ratio? At such a small scale the blade airfoil matters less due to the Reynolds number. what is the compression ratio that you are shooting for when you have the stages done?
Ray,
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