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Forum: Main CFD Forum

November 21, 2012, 00:52

Replies: 12

(Help!) Rotor Blade CFD

Views: 1,853

Posted By apoorv

Hi Have domain down stream the rotor atleast...

Hi

Have domain down stream the rotor atleast 50% of chord in case of isolated rotor.

In case of compressor rotor, I will prefer to ramp up the back-pressure from a reasonable low value to...

Forum: Main CFD Forum

November 20, 2012, 04:46

Replies: 12

(Help!) Rotor Blade CFD

Views: 1,853

Posted By apoorv

It makes difference in stablity

Hi,

If compressor it will work against pressure, turbine it has favourable pressure gradient. My tactics to handle both of them is different.

Regards

Apurva

Forum: Main CFD Forum

November 19, 2012, 23:39

Replies: 12

(Help!) Rotor Blade CFD

Views: 1,853

Posted By apoorv

Is it axial/centrifugal turbomachinery rotor blade or helicopter rotor blade

Hi

The problem you are attempting is turbomachinery or helicopter rotor. Also in case of turbomachinery is it a compressor rotor or turbine rotor

After that may be help you

Apoorv

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