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		<title>CFD Online Discussion Forums - FLUENT</title>
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			<title>CFD Online Discussion Forums - FLUENT</title>
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			<title>local nusselt for heated channel</title>
			<link>http://www.cfd-online.com/Forums/fluent/79909-local-nusselt-heated-channel.html</link>
			<pubDate>Wed, 08 Sep 2010 11:24:44 GMT</pubDate>
			<description>hi everybody, 
 
I want to calculate local Nusselt for heated channel. 
I have a constant heat flow, how to calcul Twall and T ref for each point...</description>
			<content:encoded><![CDATA[<div>hi everybody,<br />
<br />
I want to calculate local Nusselt for heated channel.<br />
I have a constant heat flow, how to calcul Twall and T ref for each point along the wall!<br />
<br />
please i need your help<br />
<br />
thank you</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>gina</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79909-local-nusselt-heated-channel.html</guid>
		</item>
		<item>
			<title>ERROR: End AOA in airfoil table too small k 1 i 1 in Fluent 6.3</title>
			<link>http://www.cfd-online.com/Forums/fluent/79906-error-end-aoa-airfoil-table-too-small-k-1-i-1-fluent-6-3-a.html</link>
			<pubDate>Wed, 08 Sep 2010 10:53:39 GMT</pubDate>
			<description><![CDATA[Hi everyone, 
 
i am using fluent 6.3 and i'm trying in generating results for a 2 bladed helicopter having 2 sections. I have the sectional lift and...]]></description>
			<content:encoded><![CDATA[<div>Hi everyone,<br />
<br />
i am using fluent 6.3 and i'm trying in generating results for a 2 bladed helicopter having 2 sections. I have the sectional lift and drag arranged in the .dat files which is similar to the standara format used in the NACA 0015. <br />
<br />
My AOA varies from -20 to 26 degrees. <br />
<br />
When i run it on Fluent i seem to get this error no matter how much i change the format.<br />
<br />
Does anyone have a idea on the matter?<br />
<br />
Thanks</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>Asela</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79906-error-end-aoa-airfoil-table-too-small-k-1-i-1-fluent-6-3-a.html</guid>
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		<item>
			<title>Velocity gradients from previous time step...</title>
			<link>http://www.cfd-online.com/Forums/fluent/79901-velocity-gradients-previous-time-step.html</link>
			<pubDate>Wed, 08 Sep 2010 09:24:30 GMT</pubDate>
			<description><![CDATA[Hi,  
 
Maybe my previous thread wasn't clear enough.  
 
I'm asking how can I access the values of velocity gradients from the previous time step......]]></description>
			<content:encoded><![CDATA[<div>Hi, <br />
<br />
Maybe my previous thread wasn't clear enough. <br />
<br />
I'm asking how can I access the values of velocity gradients from the previous time step...<br />
<br />
Thanks<br />
Mateus</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>mateus</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79901-velocity-gradients-previous-time-step.html</guid>
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		<item>
			<title>Weld pool simulation of laser-hyrid welding</title>
			<link>http://www.cfd-online.com/Forums/fluent/79900-weld-pool-simulation-laser-hyrid-welding.html</link>
			<pubDate>Wed, 08 Sep 2010 09:17:02 GMT</pubDate>
			<description>Hi, 
  
My research goal is to simulate laser hybrid weld pool by using ANSYS Fluent. I dont have much idea about this kind of simulation. Is there...</description>
			<content:encoded><![CDATA[<div>Hi,<br />
 <br />
My research goal is to simulate laser hybrid weld pool by using ANSYS Fluent. I dont have much idea about this kind of simulation. Is there any tutorial available for weld pool simulation so that I can start learning? <br />
 <br />
Regards<br />
Minhaj</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>minhaj_iut</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79900-weld-pool-simulation-laser-hyrid-welding.html</guid>
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		<item>
			<title>fluent version</title>
			<link>http://www.cfd-online.com/Forums/fluent/79894-fluent-version.html</link>
			<pubDate>Wed, 08 Sep 2010 05:57:33 GMT</pubDate>
			<description>Good Day, 
sir/madam , 
      from next month onwards i am going to be handling a project on numerical study of v2-f turbulence model for impingement...</description>
			<content:encoded><![CDATA[<div><font size="3"><font face="Times New Roman">Good Day,<br />
sir/madam ,<br />
      from next month onwards i am going to be handling a project on numerical study of v2-f turbulence model for impingement of air flow over a flat plate,  but i don't know which FLUENT version is suitable for me even i dont have more knowledge about FLUENT bcoz i m a M.tech student, and also ple let me know which meshing s/w is suitable for this project, which simulation techniques is helpfull for me.<br />
                 ple reply as soon as possible<br />
                                                   thanking you<br />
</font></font></div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>jitendra</dc:creator>
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		<item>
			<title>what does mean NV_S and NVD in UDF.</title>
			<link>http://www.cfd-online.com/Forums/fluent/79893-what-does-mean-nv_s-nvd-udf.html</link>
			<pubDate>Wed, 08 Sep 2010 04:18:00 GMT</pubDate>
			<description><![CDATA[---Quote--- 
#include "udf.h" 
DEFINE_GRID_MOTION(plate,domain,dt,time,dtime) 
{ 
 Thread *tf = DT_THREAD(dt); 
 face_t f; 
 Node *v; 
 real...]]></description>
			<content:encoded><![CDATA[<div><div style="margin:20px; margin-top:5px; ">
	<div class="smallfont" style="margin-bottom:2px">Quote:</div>
	<table cellpadding="7" cellspacing="0" border="0" width="100%">
	<tr>
		<td class="alt2">
			<hr />
			
				#include &quot;udf.h&quot;<br />
DEFINE_GRID_MOTION(plate,domain,dt,time,dtime)<br />
{<br />
 Thread *tf = DT_THREAD(dt);<br />
 face_t f;<br />
 Node *v;<br />
 real NV_VEC(omega), NV_VEC(axis), NV_VEC(dx);<br />
 real NV_VEC(origin), NV_VEC(rvec);<br />
 real sign;<br />
 int n;<br />
/* set deforming flag on adjacent cell zone */<br />
 SET_DEFORMING_THREAD_FLAG(THREAD_T0(tf));<br />
 sign = -5.0 * sin (26.178 * time);<br />
 Message (&quot;time = %f, omega = %f\n&quot;, time, sign);<br />
 <b><i><font color="navy">NV_S(omega, =, 0.0);<br />
 NV_D(axis, =, 0.0, 1.0, 0.0);<br />
 NV_D(origin, =, 0.0, 0.0, 0.152);</font></i></b><br />
 begin_f_loop(f,tf)<br />
  {<br />
   f_node_loop(f,tf,n)<br />
    {<br />
     v = F_NODE(f,tf,n);<br />
/* update node if x position is greater than 0.02<br />
and that the current node has not been previously<br />
visited when looping through previous faces */<br />
     if (NODE_X(v) &gt; 0.020 &amp;&amp; NODE_POS_NEED_UPDATE (v))<br />
      {<br />
/* indicate that node position has been update<br />
so that it’s not updated more than once */<br />
      NODE_POS_UPDATED(v);<br />
      omega[1] = sign * pow (NODE_X(v)/0.230, 0.5);<br />
      NV_VV(rvec, =, NODE_COORD(v), -, origin);<br />
      NV_CROSS(dx, omega, rvec);<br />
      NV_S(dx, *=, dtime);<br />
      NV_V(NODE_COORD(v), +=, dx);<br />
      }<br />
    }<br />
  }<br />
 end_f_loop(f,tf);<br />
}
			
			<hr />
		</td>
	</tr>
	</table>
</div>I don't know that means. I didn't find a whole day in google and UDF manual.<br />
 <br />
please explain to me..</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>oilsok</dc:creator>
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		<item>
			<title>Double layer Microchannel - Flow and Heat transfer</title>
			<link>http://www.cfd-online.com/Forums/fluent/79890-double-layer-microchannel-flow-heat-transfer.html</link>
			<pubDate>Wed, 08 Sep 2010 00:04:12 GMT</pubDate>
			<description>I am solving 3d flow and conjugate heat transfer in a double layered micro-channel.  I am considering half of the channel due to symmetry.  I have a...</description>
			<content:encoded><![CDATA[<div>I am solving 3d flow and conjugate heat transfer in a double layered micro-channel.  I am considering half of the channel due to symmetry.  I have a velocity inlet for both the layers, and a fully developed conditions( both hydro dynamically and thermally) at the outlet, so an outflow at the outlet.  I have coupled walls near the solid-fluid interface.  I have constant heat flux at the bottom of the channel.  Rest all are walls.  <br />
<br />
I am running a 3d steady, laminar case and the solution is not converging.  The mass flow rate is being balanced.  SO can anyone let me know where I am going wrong?</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>priyanka.asp</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79890-double-layer-microchannel-flow-heat-transfer.html</guid>
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		<item>
			<title>Trouble with journal file reading wall boundary condition</title>
			<link>http://www.cfd-online.com/Forums/fluent/79884-trouble-journal-file-reading-wall-boundary-condition.html</link>
			<pubDate>Tue, 07 Sep 2010 16:02:19 GMT</pubDate>
			<description>Hello All, 
 
I have created a journal file to read in a 2D case. The file is breaking down when it gets to the place where it is reading the...</description>
			<content:encoded><![CDATA[<div>Hello All,<br />
<br />
I have created a journal file to read in a 2D case. The file is breaking down when it gets to the place where it is reading the boundary conditon. The error i am getting is:<br />
<br />
no ; Shear Boundary Condition [shear-bc-noslip]: Change current value? [no] <br />
no <br />
Error: eval: unbound variable<br />
Error Object: no<br />
Invalid length<br />
<br />
When do it from the command prompt in fluent, it does not return this error.<br />
<br />
Any idea what is wrong?<br />
<br />
Thanks in advance for the help.<br />
<br />
James</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>jwillie2000</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79884-trouble-journal-file-reading-wall-boundary-condition.html</guid>
		</item>
		<item>
			<title>Two fluids at inlet</title>
			<link>http://www.cfd-online.com/Forums/fluent/79883-two-fluids-inlet.html</link>
			<pubDate>Tue, 07 Sep 2010 15:53:32 GMT</pubDate>
			<description>Hi, 
 
How to inlet two fluids at different fluids at a common inlet say into a mixing chamber???</description>
			<content:encoded><![CDATA[<div>Hi,<br />
<br />
How to inlet two fluids at different fluids at a common inlet say into a mixing chamber???</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>Haree</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79883-two-fluids-inlet.html</guid>
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		<item>
			<title>How can I implement temperature jump boundary condition in microchannel walls?</title>
			<link>http://www.cfd-online.com/Forums/fluent/79869-how-can-i-implement-temperature-jump-boundary-condition-microchannel-walls.html</link>
			<pubDate>Tue, 07 Sep 2010 10:07:10 GMT</pubDate>
			<description>Hi, 
  
I want to apply slip velocity and temperature jump boundary condition to the walls of a two-dimensional channel in Fluent.  
I use your...</description>
			<content:encoded><![CDATA[<div>Hi,<br />
 <br />
I want to apply slip velocity and temperature jump boundary condition to the walls of a two-dimensional channel in Fluent. <br />
I use your report (IFTR reports). There is not any problem for slip boundary condition but the following errors appear when I apply temperature jump to the wall:<br />
<br />
<br />
<i>Error: <br />
FLUENT received fatal signal (ACCESS_VIOLATION)<br />
1. Note exact events leading to error.<br />
2. Save case/data under new name.<br />
3. Exit program and restart to continue.<br />
4. Report error to your distributor.<br />
Error Object: ()</i><br />
<br />
<br />
<br />
<br />
I'd be grateful if someone help me.</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>sima</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79869-how-can-i-implement-temperature-jump-boundary-condition-microchannel-walls.html</guid>
		</item>
		<item>
			<title>How can I implement temperature jump boundary condition in microchannel walls?</title>
			<link>http://www.cfd-online.com/Forums/fluent/79868-how-can-i-implement-temperature-jump-boundary-condition-microchannel-walls.html</link>
			<pubDate>Tue, 07 Sep 2010 10:06:10 GMT</pubDate>
			<description>Hi  everyone, 
  
I want to apply slip velocity and temperature jump boundary condition to the walls of a two-dimensional channel in Fluent.  
There...</description>
			<content:encoded><![CDATA[<div>Hi  everyone,<br />
 <br />
I want to apply slip velocity and temperature jump boundary condition to the walls of a two-dimensional channel in Fluent. <br />
There is not any problem for slip boundary condition but the following errors appear when I apply temperature jump to the wall:<br />
<br />
<br />
<i>Error: <br />
FLUENT received fatal signal (ACCESS_VIOLATION)<br />
1. Note exact events leading to error.<br />
2. Save case/data under new name.<br />
3. Exit program and restart to continue.<br />
4. Report error to your distributor.<br />
Error Object: ()</i><br />
<br />
<br />
<br />
<br />
I'd be grateful if help me.</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>sima</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79868-how-can-i-implement-temperature-jump-boundary-condition-microchannel-walls.html</guid>
		</item>
		<item>
			<title>problem with heat flux in the wall</title>
			<link>http://www.cfd-online.com/Forums/fluent/79865-problem-heat-flux-wall.html</link>
			<pubDate>Tue, 07 Sep 2010 08:52:54 GMT</pubDate>
			<description>Hello 
I am modeling a plate fin heatsink in fluent,when i apply constant heat flux for example 200 w/m^2 to the base plate  there is no heat...</description>
			<content:encoded><![CDATA[<div>Hello<br />
I am modeling a plate fin heatsink in fluent,when i apply constant heat flux for example 200 w/m^2 to the base plate  there is no heat transfer between the solid heatsink and the fluid flow and there is no difference between inlet and outlet temperatures,but when instead of heat flux i apply &quot;heat generation&quot; to the base plate,in this case there is heat transfer between heatsink and fliud flow, and the temperature of inlet and outflow differs,do you have any idea what is the problem with heat flux?<br />
Thanks</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>gholamghar</dc:creator>
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		<item>
			<title>Velocity gradient in previous timestep</title>
			<link>http://www.cfd-online.com/Forums/fluent/79863-velocity-gradient-previous-timestep.html</link>
			<pubDate>Tue, 07 Sep 2010 08:47:19 GMT</pubDate>
			<description>Hi,  
 
I need to write an UDF where velocity gradients in current and previous timestep are included.  
 
As far as I understand gradients from...</description>
			<content:encoded><![CDATA[<div>Hi, <br />
<br />
I need to write an UDF where velocity gradients in current and previous timestep are included. <br />
<br />
As far as I understand gradients from previous timestep cannot be called directly (like for the current time - for example C_DUDX(c,t)). I guess the easiest way (the only way) is to use velocity from previous time step (<font size="+0">C_U_M1(c,t)</font>) and calculate the gradient... But I cannot find a macro for the cell size... and also what happens when I use unstructured mesh? <br />
Where is it written how Fluent calculates the velocity gradient?<br />
<br />
Thanks, <br />
Mateus</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>mateus</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/fluent/79863-velocity-gradient-previous-timestep.html</guid>
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		<item>
			<title>air entrainment in fluent</title>
			<link>http://www.cfd-online.com/Forums/fluent/79858-air-entrainment-fluent.html</link>
			<pubDate>Tue, 07 Sep 2010 06:38:16 GMT</pubDate>
			<description>Hellow   I want  to  model HYDRAULIC  JUMP (including  air entrainment)  with  FLUENT . Can fluent  do This  work.</description>
			<content:encoded><![CDATA[<div><font face="Calibri"><font size="3">Hellow   I want  to  model HYDRAULIC  JUMP (including  air entrainment)  with  FLUENT . Can fluent  do </font></font><font size="3"><font face="Calibri">This  work.  </font></font></div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>hamedarshadi</dc:creator>
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		<item>
			<title>Coloring of particles</title>
			<link>http://www.cfd-online.com/Forums/fluent/79857-coloring-particles.html</link>
			<pubDate>Tue, 07 Sep 2010 06:37:58 GMT</pubDate>
			<description><![CDATA[Hello 
  
I have 5 spherical balls of different diameter being injected in the pipe But the color of all the balls are same when i click on "display"...]]></description>
			<content:encoded><![CDATA[<div>Hello<br />
 <br />
I have 5 spherical balls of different diameter being injected in the pipe But the color of all the balls are same when i click on &quot;display&quot; in the &quot;particle tracks&quot; with &quot;particle variables color by particle diamter.<br />
 <br />
Could anyone please guide me how can i change the color of the balls with respect to diameter so that its easy to visulaize. <br />
 <br />
Thanks<br />
Mohsin</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/fluent/">FLUENT</category>
			<dc:creator>Mohsin</dc:creator>
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