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June 15, 2010, 11:04 

#101 
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Join Date: Jan 2010
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Hi nana,
Thanks for help, at moment i'm doing some simulaiton with a mesh with bounday layer, as sagarmatha advised me. He looks one case and data file i sent to him and he found some wrong on y+ function. Hope this could be the solution. I have some questions, what do u mean when u said "I also have the negative TSR for my previous simualtion when i mointor the Cm"? Can u share with me the condition are u using? Like rpm and tsr? and the result u obtained? and the last one, how do u obtain the average moment after some rotation? Thanks again. 

June 16, 2010, 22:00 

#102 
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Join Date: Jul 2009
Posts: 43
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Hi esp:
I do not think bounday layer is suitable for the case, and based on my own experience, y+ value won't affect much even you try the BL. I have tried different y+ value with different set of mesh before, but it seems not much difference. However, if you want to try to prove, jsut try it. I think the msot error is based on the BC set up. Well, you can give me your email address, i can send my Cm plot to you ok. 

June 17, 2010, 02:32 

#103  
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sagarmatha
Join Date: Apr 2010
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Quote:
also, y+ is a critical parameter to monitor for good nearwall mesh. if you are using fluent, it suggests a y+ of 30300 for standard wall functions and y+ average of 1 (with no values exceeding 5) for enhanced wall treatment. the reason why it is important to have a good nearwall mesh is that if you assume a fluid element with shear and pressure forces acting on it, the one responsible for the rotation of the fluid element is the shear. where do you get shear? in may cases, if you have a wall, you will definitely encounter shear forces on the wall that cause your fluid elements to rotate. this is a very important factor in the behavior of the fluid past a wall. this has massive effects on the factors that give lift and drag to a blade. for a static airfoil case, you may not experience significant differences in the results. but for a pitching and plunging airfoil, lift prediction is very sensitive to near wall mesh. even the prediction of flow behavior dramatically changes with different near wall meshes. if you ignore y+, you dont know if your simulation results are sensible or not. also, some turbulence models are sensitive to y+, especially those that try to predict laminarturbulent transition on walls. 

June 17, 2010, 23:12 

#104 
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Hi Sagarmatha:
I totally agree that y+ is important when chooseing the turbulence model. I also agree that different y+ value need the different turbulence scheme for better and accurate results. However, I have tried with different Y+ value like Y+=1 using the enhance wall boundary method and also Y+=30~500 using standard wall function to see the difference. The trend is the same, only a bit difference shows in the results. Of course, if you want to see the bounday layer and also the blade interaction, that one is crucial. I jsut say that based on my own simualtion results. 

June 30, 2010, 16:12 
Using sliding mesh for VAWT

#105 
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SOhail
Join Date: Jun 2010
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Hi all,
I am working on 2D simulation of VAWT using gambit and fluent. I started my work by creating mesh file for single airfoil in vertical motion. I created a central stationary mesh then a circular mesh strip around it which contains airfoil & which would be moving, then i created interface region (again a circular strip) around the moving mesh and finally a big rectangular domain of about 30 times the chord which is stationary mesh. i used velocity inlet for inlet region and pressure outlet for outlet region and pressure farfield for upper and lower edge of rectangular domain and wall for airfoil, but i dont know what BC should i use for interface region in between and in fluent how should i rotate the mesh with some angular velocity so that airfoil would rotate. I read somewhere that we need to write a UDF for that?? Initially i want to compute for flow coming in with Re=10^6 and blades are rotating with 60rpm. i would be glad if anyone could help me out. Thanks and Regards. 

June 30, 2010, 16:41 

#106  
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sagarmatha
Join Date: Apr 2010
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Quote:
regarding your mesh, how come you are using more than one interface region (one between the central domain and the rotating mesh and the other one between the rotating mesh and the outer domain)? using interface regions introduces numerical errors and noise in the computation (fluent interpolates values when nodes do not coincide at specific points in time during the sliding). so you must use it only when necessary. why not attach the central domain to the rotating domain and let that rotate as well. put a center post to include the effects of the post on the wake downwind. regarding BCs, if you are using farfield on two boundaries, why not use farfield on all? specify velocity as a function of mach number. enable energy equation, use ideal gas for air density. see to it you are aware of the temperature setting as speed of sound in dry air is dependent on temperature. if you do this (specifying farfield on all boundaries), you will avoid reverse flow warnings on your fluent run. just be sure your boundaries are far enough. your 30 chord lengths distance does not give us a good picture because you have not told us your vawt diameter, airfoil chord, or vawt solidity. in defining interface regions, do a back read. it has been posted already. you do not need a udf unless you want variable angular velocity. for constant angular velocity, moving mesh with rotational motion defined is sufficient. 

June 30, 2010, 17:09 
VAWT dimensions

#107 
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SOhail
Join Date: Jun 2010
Posts: 16
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Hi sagar,
I am starting my simulations with a smaller VAWT in order to save computation time, My VAWT has diameter of 4. I am searching for posts related to how to move mesh for VAWT in the same thread. I was following fluent tutorial for preparing mesh for sliding mesh, which uses a interface region between stationary grid and moving grid so i did the same, but i experienced some error using interface, when i am actually initializing the problem in fluent it gives a warning that periodicity for interface region is not set. what does that mean? can you help me out? And how can i rotate grid with out using interfaces. Please help me out Buddy. Thanks for your reply. 

June 30, 2010, 21:45 
Periodic zone for grid interface

#108 
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SOhail
Join Date: Jun 2010
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Hi all,
I am working with VWT 2D simulation, i am using moving mesh method to rotate airfoil, i created stationary mesh for center region and am moving the grid around airfoil, but when im initializing the problem in fluent it gives an error that no periodic zone adjacent to grid interface, i have no clue what does that mean, can anyone help me out please?? Thanks 

July 29, 2010, 03:38 

#109 
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Join Date: Jul 2009
Posts: 43
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Dear all:
Is there any one doing helical twist blade profile for VAWT. How should i make that turbine blade profile? Anyone can give me some idea? I need to do the numerical simualtion on that trubine and study the turbine performance. I really appreciate that anyone can provide some information on that. Thanks 

July 30, 2010, 00:30 

#110 
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Hi Sagarmatha:
I am doing validation study for the 3D VAWT with 3 straight blade. I have do the simuation using Fluent to compare the Cp with TSR with one journal paper. The blade profile is NACA 0022 and with chord 100mm and span 400mm. The rotor diameter is arond 600mm. I have tried to mointor the moment coefficient around 10 revoultion using ke RNG and kw SST to compare the results with 2 wind speed at 5.07m/s and 5.81m/s from TSR = 2.1 to TSR=2.5. However, i have negative cm when TSR increased to 2.4 and 2.5. I change the time step to 0.001, then i can get the positive cm. Now i am trying to use SA (my prof ask me to try) with the same set up, howver i have negative cm at TSR=2.4 and TSR=2.5. Why it has the negative value. Do you have any suggestion? I thins the One possibility is becasue the moment will be drop when the turbine rotational speed reach its maximum. However, the SST and RNG turbulence model gives the positive cm. I am a bit lost now. Kindly hope that u can give any suggestion. Really appreciate on yr help. 

August 11, 2010, 11:40 
2d VAWT

#111 
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Join Date: Aug 2010
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Hi all,
for the rotating mesh for VAWT is it similar to the tenth tutorial? I have set up in GAMBIT a NACA 0012. There are the outer and inner regions which is stationary and a denser circular part in which the blade is placed. Do I set up walls in Gambit and then redefine them as interiors like in the tutorial? I have tried simulating in FLUENT once but I think my blade is stationary and the circular fluid is rotating. The tutorial has a small section where one defines the blade as rotating with the surrounding zone but I'm not sure how this works as I never made any relationship between the blade and the rotating section. Any assistance would be appreciated greatly. Conor, MSc Student 

August 25, 2010, 21:56 

#112 
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Join Date: Jul 2009
Posts: 43
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Hi Esp:
Have you still working on the VAWT tubrine? I have negative moment coefficient. I think you meet this problem before is it ? Have you figure it out, is there any suggestion to solve it? Thanks a lot. 

September 19, 2010, 06:08 

#113 
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Join Date: Feb 2010
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Hello Everyone,
I am working on my Thesis which is basically 2D CFD simulation of Vertical Axis Wind Turbine and comparing my results with "Wind tunnel and numerical study of a small vertical axis wind turbine" by Robert Howell et al. I need to calculate the torque generated by a wind turbine in order to find Cp. In this regard I am running 2D simulation with sliding mesh technique and saving the case/data file after every 10 degrees of rotation hence I have 36 files for one complete revolution. Now I am reporting the value of forces in X and Y direction (Fx and Fy) from each case/data file for all 3 Blades. Then I calculate Torque on each blade using formula T1 =  Fx1.RcosΘ  Fy1.R.sinΘ T2 = Fx2.Rcos(Θ+120)  Fy2.R.sin(Θ+120) T3 = Fx3.Rcos(Θ+240)  Fy3.R.sin(Θ+240) Total Torque T = T1 + T2 + T3 (Total Torque “T” is calculated for every 10 degree of rotations) Average Torque = Σ T/n (0360 degrees) where n = 360/10 = 36 Please let me know if the method I am using is correct. I am confused about the sign convention of Torque equations. is there any other way to find out Torque and Cp(Coefficient of performance)? [/IMG]. Last edited by jola; January 5, 2012 at 12:03. 

March 14, 2011, 00:36 
helical twist blade

#114  
New Member

Quote:
hopefully it can help you,sorry for my english 

April 20, 2011, 16:43 

#115 
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Ahmad Zein
Join Date: Feb 2011
Posts: 4
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Hello,
I am working on a 2D ANSYS simulation for a 3 bladed VAWT. After the solution converges the moment values are totaly wrong and the contours show that the stationary zone is not interacting with the moving zone.I would like to ask any one to explain for me what is the problem and provid me with a solution. Thank you and best regards 

February 6, 2012, 00:37 
sliding mesh

#116 
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Join Date: Jan 2012
Posts: 58
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hello
i had the problem in sliding mesh in case of train traveling in tunnel . can any one help me plz. my email is sheikhnasir39@gmail .com thanks with regards 

July 16, 2012, 06:15 
Sliding mesh  VAWT

#117 
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dalecooper
Join Date: Jul 2012
Posts: 10
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Hello, I'm a new user of CFX currently working in simulating VAWT in 2D for my master thesis. I have been searching and actually I'm a bit confused trying to put in clear some points.
I've constructed the geometry of the blades in 2D with Ansys Design Modeller and I don't know which is the procedure to simulate a sliding mesh in CFX. I've begun with ICEM CFD, but don't know if that is the best option. One of my doubts consist if this has something to do with the "Rotating Frame of Reference" option in CFXPre. Thanks in advance for any kind of help. Best regards. Last edited by dalecooper; July 17, 2012 at 10:49. 

September 5, 2012, 06:48 
VAWT Sliding mesh

#118 
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Join Date: Jul 2012
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If you're still working on this you may want to have a look at http://www.pdslimited.com/index_file...rbine_VAWT.htm which is a 3D analysis


January 14, 2013, 16:04 

#119 
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bhushan patil
Join Date: May 2012
Posts: 19
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dear frnds plz tell me how to calculate torque in fluent i am working on vertical axis wind turbine H shaped darruis type so for that concern i am doing 2d simulations unsteday for that i am giving cl ,cd cm moniters on blades so will plz tell me how to find out direct torque in fluent or how to corelate it 2 moment i am attching paper and some images of my mesh so it will clear u problem
plz tell me it needs udf to find torque on blades Last edited by p.bhushan2727@gmail.com; January 14, 2013 at 16:19. 

May 4, 2013, 03:07 
Negative moment

#120 
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Reza
Join Date: Sep 2010
Posts: 9
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Hello
I work on a 4bladed VAWT (Savonius). My analysis is Steady and 3D. The wind velocity is 10 m/s. this Rotor has 4 blades that each one has a semicircle section. And the radius of the rotor is 10m (It's very large) The obtained moment from analysis is negative and low. I don't have any experimental data. Why the moment is low and negative, while the rotor is very big and wind velocity is 10????? I'm very anxious, Please help me, Thanks so much all the best wishes 

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