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			<title>air hammer in aerostatic bearing</title>
			<link>http://www.cfd-online.com/Forums/main/79912-air-hammer-aerostatic-bearing.html</link>
			<pubDate>Wed, 08 Sep 2010 12:16:27 GMT</pubDate>
			<description>why air hammer appears in aerostatic bearing ?  it mainly depends on the volume of the pocket/recess? please help me, thank you.</description>
			<content:encoded><![CDATA[<div>why air hammer appears in aerostatic bearing ?  it mainly depends on the volume of the pocket/recess? please help me, thank you.</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/main/">Main CFD Forum</category>
			<dc:creator>spcwin</dc:creator>
			<guid isPermaLink="true">http://www.cfd-online.com/Forums/main/79912-air-hammer-aerostatic-bearing.html</guid>
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			<title>gas diffusion through membrane</title>
			<link>http://www.cfd-online.com/Forums/cfx/79911-gas-diffusion-through-membrane.html</link>
			<pubDate>Wed, 08 Sep 2010 12:14:33 GMT</pubDate>
			<description>Lets say we have a box where there is a source of gas CO2 (at the bottom) and it is shut by a membrane (top). The box with the membrane  is in...</description>
			<content:encoded><![CDATA[<div>Lets say we have a box where there is a source of gas CO2 (at the bottom) and it is shut by a membrane (top). The box with the membrane  is in atmospheric environment (simplest case). I want to simulate in CFX the diffusion through the membrane and finally find out the mass fractions of the air and CO2 inside the box.<br />
<br />
I create two domains: the bottle without the membrane and the membrane itself. The first one is a fluid domain defined to contain a mixture of air (constraint) and CO2 with the kinematic diffusivity of CO2 in air.<br />
<br />
What i did was to define the membrane domain as fluid domain containing again the CO2 and Air(constraint) mixture but with different kinematic viscocity. <br />
<br />
There is a common area (between box domain and membrane domain) though that i do not know whether to define as a boundary or as an interphase (i did it as an interphase and the solution has errors - i get no results) <br />
<br />
Any help on this?<br />
<br />
What type of domain should i define the membrane?<br />
<br />
If solid then i can not find a way to insert the diffusion coefficient of the membrane interacting with the mixture</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/cfx/">CFX</category>
			<dc:creator>sosat1012</dc:creator>
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			<title>I need help for TUI command</title>
			<link>http://www.cfd-online.com/Forums/fluent/79910-i-need-help-tui-command.html</link>
			<pubDate>Wed, 08 Sep 2010 11:49:36 GMT</pubDate>
			<description>Hi, everybody. 
    I am writing a TUI journal. For the journal, one of the task is to creat a point-surface monitor. I know how to creat it. But I...</description>
			<content:encoded><![CDATA[<div>Hi, everybody.<br />
    I am writing a TUI journal. For the journal, one of the task is to creat a point-surface monitor. I know how to creat it. But I can't find the command to change the type of X Axis variate. As the following pic shows,<br />
<img src="http://www.cfd-online.com/Forums/attachments/fluent/4646d1283946083-i-need-help-tui-command-1.jpg" border="0" alt="" /><br />
 I want to change &quot;Iteration&quot; to &quot;Flow time&quot; for &quot;X Axis&quot;, and it should &quot;Get Data Every&quot; &quot;Time Step&quot;. <br />
    I don't know which TUI command I should use. Anyone could help me?<br />
    Thanks.</div>


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			<dc:creator>ringtail</dc:creator>
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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>
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			<title>parallel and multiphase</title>
			<link>http://www.cfd-online.com/Forums/cfx/79908-parallel-multiphase.html</link>
			<pubDate>Wed, 08 Sep 2010 11:24:15 GMT</pubDate>
			<description><![CDATA[hello, 
i have a problem, 
my calculation on 4 cpu's differs two much from this on 8 cpu's with the same setup? what did go wrong? (multiphase flow)]]></description>
			<content:encoded><![CDATA[<div>hello,<br />
i have a problem,<br />
my calculation on 4 cpu's differs two much from this on 8 cpu's with the same setup? what did go wrong? (multiphase flow)</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/cfx/">CFX</category>
			<dc:creator>Zaktatir</dc:creator>
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			<title>GT-Power - Star-CCM+ Coupling</title>
			<link>http://www.cfd-online.com/Forums/star-ccm/79907-gt-power-star-ccm-coupling.html</link>
			<pubDate>Wed, 08 Sep 2010 10:59:11 GMT</pubDate>
			<description><![CDATA[Hello, 
I'm trying to couple GT-Power and Star-CCM+ (my versions are avaible for that) and I have no experience for that. 
Has someone a tutorial...]]></description>
			<content:encoded><![CDATA[<div>Hello,<br />
I'm trying to couple GT-Power and Star-CCM+ (my versions are avaible for that) and I have no experience for that.<br />
Has someone a tutorial about this topic ? Or can someone give me some tipps about this subject ?<br />
Thank you in advance<br />
Best regards</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/star-ccm/">STAR-CCM+</category>
			<dc:creator>sheintz</dc:creator>
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		<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>
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		</item>
		<item>
			<title>System time overhead in OF</title>
			<link>http://www.cfd-online.com/Forums/openfoam/79905-system-time-overhead.html</link>
			<pubDate>Wed, 08 Sep 2010 10:42:03 GMT</pubDate>
			<description>Hi all, 
 
I have noticed that on our cluster that openfoam have a very different cpu usage compared to other cfd codes. 
 
In OF a large fraction of...</description>
			<content:encoded><![CDATA[<div>Hi all,<br />
<br />
I have noticed that on our cluster that openfoam have a very different cpu usage compared to other cfd codes.<br />
<br />
In OF a large fraction of the time is spend in system cpu time compared  to user cpu time. Other cfd codes we have had our hands on spend almost  100% of the time in user cpu.<br />
<br />
I have made a small case based on the angledDuct case with 178000 cells  using simpleFoam. The case was constructed so no IO was performed.<br />
<br />
In serial more than 30% of the time is spend in system time. Is this an overhead due to the dynamic memory allocation in OF?<br />
<br />
<a href="http://www.cfd-online.com/Forums/attachments/openfoam/4644-system-time-overhead-simplefoam_job.jpg" target="_blank" title="Name:  
Views: 
Size:  ">Attachment 4644</a><br />
<br />
When running the case in parallel (2 nodes) the system time CPU time fraction drops to a few percent which is difficult for me to understand.<br />
<br />
<a href="http://www.cfd-online.com/Forums/attachments/openfoam/4645-system-time-overhead-simplefoam_job2.jpg" target="_blank" title="Name:  
Views: 
Size:  ">Attachment 4645</a><br />
<br />
Can anyone explain the apparent serial overhead?<br />
<br />
Best regards,<br />
                    Ask</div>


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			<category domain="http://www.cfd-online.com/Forums/openfoam/">OpenFOAM</category>
			<dc:creator>askjak</dc:creator>
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			<title>Nv-s ?? Nv-d ?? Help!!!</title>
			<link>http://www.cfd-online.com/Forums/fluent-udf/79904-nv-s-nv-d-help.html</link>
			<pubDate>Wed, 08 Sep 2010 10:33:26 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-udf/">Fluent UDF and Scheme Programming</category>
			<dc:creator>oilsok</dc:creator>
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			<title>Environment variable in linux</title>
			<link>http://www.cfd-online.com/Forums/star-ccm/79903-environment-variable-linux.html</link>
			<pubDate>Wed, 08 Sep 2010 10:08:45 GMT</pubDate>
			<description><![CDATA[:confused:When I install star-ccm+ successfully, it didn't work well, there is something wrong. someone said when star-ccm+ installed, I must  set...]]></description>
			<content:encoded><![CDATA[<div>:confused:When I install star-ccm+ successfully, it didn't work well, there is something wrong. someone said when star-ccm+ installed, I must  set the environment variable, but i knew linux very little,could someone tell me how to set the environment variable? Thanks!</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/star-ccm/">STAR-CCM+</category>
			<dc:creator>xinzhiyu2008</dc:creator>
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			<title>OF1.6.x:localBlended schemes missing correction funtions</title>
			<link>http://www.cfd-online.com/Forums/openfoam-bugs/79902-of1-6-x-localblended-schemes-missing-correction-funtions.html</link>
			<pubDate>Wed, 08 Sep 2010 10:01:16 GMT</pubDate>
			<description><![CDATA[Hello everyone, 
 
when comparing fixedBlended.H and localBlended.H then localBlended is missing the member functions "correction" and "corrected"....]]></description>
			<content:encoded><![CDATA[<div>Hello everyone,<br />
<br />
when comparing fixedBlended.H and localBlended.H then localBlended is missing the member functions &quot;correction&quot; and &quot;corrected&quot;. These should be necessary when using e.g. linearUpwind as one of the two blending schemes.<br />
I attached a suggested fix, where I copied the two member functions with a little adjustment because the blending factor in localBlended.H is a field.<br />
<br />
Best Regards<br />
Dominik Christ<br />
<br />
<br />
P.S.: Thanks to Sven Degner and Ulf Bunge who discovered this bug.</div>


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	<td><a href="http://www.cfd-online.com/Forums/attachments/openfoam-bugs/4641d1283939983-of1-6-x-localblended-schemes-missing-correction-funtions-localblended.h">localBlended.H</a> (6.6 KB)</td>
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			<category domain="http://www.cfd-online.com/Forums/openfoam-bugs/">OpenFOAM Bugs</category>
			<dc:creator>dominik_christ</dc:creator>
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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>
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			<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>
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			<title>Good Universities for MS in CFD (in US and UK both)</title>
			<link>http://www.cfd-online.com/Forums/main/79899-good-universities-ms-cfd-us-uk-both.html</link>
			<pubDate>Wed, 08 Sep 2010 08:52:26 GMT</pubDate>
			<description>Hello guys, I am looking forward for MS (Fall 2k11). Can you please suggest me the universities in US that have research interests in the field of...</description>
			<content:encoded><![CDATA[<div>Hello guys, I am looking forward for MS (Fall 2k11). Can you please suggest me the universities in US that have research interests in the field of CFD.</div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/main/">Main CFD Forum</category>
			<dc:creator>vinaynitrkl</dc:creator>
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			<title>How I could import Ansys mesh into CFX?</title>
			<link>http://www.cfd-online.com/Forums/ansys-meshing/79898-how-i-could-import-ansys-mesh-into-cfx.html</link>
			<pubDate>Wed, 08 Sep 2010 08:43:17 GMT</pubDate>
			<description><![CDATA[Dears, 
 
I wanna import ansys mesh into CFX (I have ansys 12). I can import the mesh, but I can't define the boundary condition, because CFX...]]></description>
			<content:encoded><![CDATA[<div>Dears,<br />
<br />
I wanna import ansys mesh into CFX (I have ansys 12). I can import the mesh, but I can't define the boundary condition, because CFX consider whole geometry as a block. Could u plz help me?<br />
<br />
<a href="mailto:m.shahverdi@gmail.com">m.shahverdi@gmail.com</a></div>

]]></content:encoded>
			<category domain="http://www.cfd-online.com/Forums/ansys-meshing/"><![CDATA[Ansys Meshing & Geometry]]></category>
			<dc:creator>mahdi57</dc:creator>
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