blade interface for unsteady computation

June 11, 2003, 04:27

Hi all,

i have a question about the blade interface. Normally, the numbers of stator and rotor blades in turbomachinery are not equal. To conduct an unsteady simulation, the blade interface should be matched to each other. I've heard about some scaling methods to solve this problem. Can anyone tell me in detail or give me some references?

I thank you very much in advance.

wang

June 11, 2003, 11:44

there are couple of techniques for this kind of problems. one is developed by Erdos J.I. refer to his AIAA paper. The otherone which will i think be suitable for your case is developed by Rai M. M. you can refer to AIAA journal for his paper

J-

June 11, 2003, 13:02

Look for J.D. Dentons and W.N. Dawes paper in Journal of turbomachines particularly 1992.

June 11, 2003, 04:27	blade interface for unsteady computation	#1
wang Guest Posts: n/a	Hi all, i have a question about the blade interface. Normally, the numbers of stator and rotor blades in turbomachinery are not equal. To conduct an unsteady simulation, the blade interface should be matched to each other. I've heard about some scaling methods to solve this problem. Can anyone tell me in detail or give me some references? I thank you very much in advance. wang

June 11, 2003, 11:44	Re: blade interface for unsteady computation	#2
centaur_ks Guest Posts: n/a	there are couple of techniques for this kind of problems. one is developed by Erdos J.I. refer to his AIAA paper. The otherone which will i think be suitable for your case is developed by Rai M. M. you can refer to AIAA journal for his paper J-

June 11, 2003, 13:02	Re: blade interface for unsteady computation	#3
A.S. Guest Posts: n/a	Look for J.D. Dentons and W.N. Dawes paper in Journal of turbomachines particularly 1992.

Similar Threads
Thread	Thread Starter	Forum	Replies	Last Post
Wind turbine simulation	Saturn	CFX	60	July 17, 2024 06:45
RPM in Wind Turbine	Pankaj	CFX	9	November 23, 2009 05:05
Convective Heat Transfer - Heat Exchanger	Mark	CFX	6	November 15, 2004 16:55
blade interface for unsteady computation	wang	CFX	1	June 11, 2003 19:33
Replace periodic by inlet-outlet pair	lego	CFX	3	November 5, 2002 21:09