|October 12, 2006, 10:55||
blade passage flow
I have got an incompressible flow (M<0.2) model built for a sector blade passage with a clearance present between the blade and the outer casing. I got the complete test information (profile) right from inlet to the exit.
For this case I tried giving inlet total pressure and exit static pressure profiles to calculate the mass flow and I found it is 20% less. I'have checked with the density, which is constant.
Can someone suggest me to know what boundary conditions can I really fit and kind of turbulence model I can use to simulate one blade passage to match the test.
Regards Thanks in advance Babu
|Thread||Thread Starter||Forum||Replies||Last Post|
|Flow meter Design||CD adapco Group Marketing||CD-adapco||3||June 21, 2011 08:33|
|Re: how to do this turbine blade passage flow nanl||manish||NUMECA||1||November 3, 2006 00:01|
|transform navier-stokes eq. to euler-eq.||pxyz||Main CFD Forum||37||July 7, 2006 08:42|
|Re: how to do this turbine blade passage flow nanl||manish||Phoenics||1||February 21, 2006 10:59|
|Re: how to do this turbine blade passage flow nanl||manish||CD-adapco||0||January 12, 2006 12:37|