|May 24, 2007, 14:31||
2D Compressor cascade study using DFLVR blade
i am analysing 2D compressor cascade using DFLVR blade, by varying its leading edge i am unable to find any standard test run of this blade,
if any one has done 2d-COMPRESSOR sTUDY THEN PLS HELP, i am facing a problem, in the result i am getting, i am using unstructured grid, inflow parameter as Pressure farfied(i am stimulating COmpressive flow at mach 1.4) and using a alue of 101325 pascal. and outflow as 1000pascal. i am using spalar allmaras scheme.
i am not getting good results. and also the grid is pretty schewed.
it would be great if i get some standard run case. which i can follow. its urgent.
i have to finish the work in 2 weeks
thanks in advance
|Thread||Thread Starter||Forum||Replies||Last Post|
|Calculating lift force of a wind turbine blade problem||LittleBart||CFX||4||June 29, 2011 02:33|
|Rotating blade in circular/square vessel (Salome+OpenFoam)||voingiappone||OpenFOAM||0||May 19, 2011 11:38|
|how to study a simple rotating blade?||signofra||CFX||1||April 1, 2010 06:23|
|Meshing a 3D, tapered and twisted blade with Gambit-TGrid||teskio||ANSYS Meshing & Geometry||0||July 3, 2009 10:36|
|Flow study through Turbine Blade passage||Subrata||FLUENT||1||May 4, 2007 11:28|