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September 19, 2013, 05:10 |
boundary layer development in gambit
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#1 |
New Member
maaz ahmad
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Location: india
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i am working on wind effects on high rise building..i have to develop boundary layer along the wall on computational domain and building as well...gambit is showing message..initialization failed...with error code 1...i am unable to resolve this..kindly help me...
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September 19, 2013, 06:16 |
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#2 |
Super Moderator
Maxime Perelli
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more info please, with pictures
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In memory of my friend Hervé: CFD engineer & freerider |
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September 20, 2013, 02:25 |
kindly help me out...
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#3 |
New Member
maaz ahmad
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Location: india
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hi max..
i have to develop boundary layer on the ground and building surface..i am attaching pics here,, kindly look into it.. and help me ..out..thanx whole computational domain.jpg computational domain from different angles.jpg high rise building.jpg |
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September 20, 2013, 02:33 |
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#4 |
Super Moderator
Maxime Perelli
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then pick surfaces of ground and building...
take care of first cell's height. If you give an exotic value, then the BL propagation may fail http://aerojet.engr.ucdavis.edu/gamb..._blayer_create
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In memory of my friend Hervé: CFD engineer & freerider |
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September 21, 2013, 04:19 |
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#5 |
New Member
maaz ahmad
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max thanx for your response...i have changed the geometry of computational domain to resolve the error..
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September 23, 2013, 04:33 |
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#6 |
New Member
maaz ahmad
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max.. can you tell me about the aspect ratio for boundary layer ....
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September 23, 2013, 04:49 |
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#7 |
Super Moderator
Maxime Perelli
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http://aerojet.engr.ucdavis.edu/gamb...spec_algorithm
with aspect ratio algorithm, you don't have fixed first cell' s height.
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In memory of my friend Hervé: CFD engineer & freerider |
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September 24, 2013, 00:32 |
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#8 |
New Member
maaz ahmad
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no dear the thing i wanna ask is that when we examine the mesh and in the option of quality type we click aspect ratio , then what is the range of this value that is best suited for a mesh.
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September 24, 2013, 02:34 |
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#9 |
Super Moderator
Maxime Perelli
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from Help: "However, a general rule of thumb is to avoid aspect ratios in excess of 5:1. " --> http://aerojet.engr.ucdavis.edu/flue...ug/node155.htm
I would simply load the mesh in the solver and run a check mesh
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In memory of my friend Hervé: CFD engineer & freerider |
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September 27, 2013, 03:51 |
problem in udf for velocity proflie
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#10 |
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maaz ahmad
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/************************************************** *********************
vprofile.c UDF for specifying steady-state velocity profile boundary condition ************************************************** **********************/ #include "udf.h" DEFINE_PROFILE(inlet_x_velocity, thread, position) { real x[ND_ND]; /* this will hold the position vector */ real y; face_t f; begin_f_loop(f, thread) { F_CENTROID(x,f,thread); y = x[1]; ( F_PROFILE(f, thread, position) = (10 + y/12.5)*cos(5.0/180.*3.1415927); } end_f_loop(f, thread) } DEFINE_PROFILE(inlet_y_velocity, thread, position) { /* insert your own code here*/ } max....in this udf while defining F_PROFILE(f, thread, position) = (10 + y/12.5)*cos(5.0/180.*3.1415927); can we use log formula also, if yes then please explain it for me..... |
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September 27, 2013, 05:05 |
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#11 | |
Senior Member
Rick
Join Date: Oct 2010
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Quote:
see attached picture from udf manual. Daniele |
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