|
[Sponsors] |
![]() |
![]() |
#1 |
Guest
Posts: n/a
|
Hello,
I am a first year PhD student in Mechanical engineering at the University of Strathclyde UK. Presently i am doing two-dimensional flow analysis of an uncooled gas turbine. I have made a two-dimensional T.6 model of a stator with circular camber line in gambit. I want to ask how to place the periodic boundaries. Are these midway between two blade sections. Is a periodic boundary copy of circular camber line. Please also tell if it is correct if I connect the periodic boundary with the outlet boundary by a straight line having outlet flow angle. Thank you, Regards, M.Usman |
|
![]() |
![]() |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
1d analysis and simulation of gas turbine power plant | sridhar.d009 | FLUENT | 0 | September 28, 2010 07:46 |
1D analysis and simulation of gas turbine power plant | sridhar.d009 | Main CFD Forum | 1 | September 28, 2010 07:38 |
Constant velocity of the material | Sas | CFX | 15 | July 13, 2010 08:56 |
blade analysis of gas turbine | Fayyaz Husain | Main CFD Forum | 1 | March 3, 2010 01:13 |
Gas pressure question | Dan Moskal | Main CFD Forum | 0 | October 24, 2002 22:02 |