<?xml version="1.0" encoding="UTF-8"?><rss xmlns:dc="http://purl.org/dc/elements/1.1/" xmlns:content="http://purl.org/rss/1.0/modules/content/" xmlns:atom="http://www.w3.org/2005/Atom" version="2.0"><channel><title><![CDATA[新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题]]></title><description><![CDATA[<p dir="auto">在网上找了很久没有发现有关的解决方法。所以才来请大家能给点指点意见。<br />
现在想用openFOAM模拟冲击波管喷出的低马赫数冲击波的密度计测。<br />
边界条件和其他的文件基本copy的tutorial里的nacaAirfoil，关于U文件夹里的internalfield的值是什么意思？然后如果用supersonicfreestream该怎么设定<br />
p的inlet和outlet该怎么设定（如果用waveTransmissive）<br />
这几项需要注意什么请指教下，万分感谢！</p>
]]></description><link>https://cfd-china.com/topic/1045/新手求问冲击波管喷出的低马赫数supersonic的-边界条件问题</link><generator>RSS for Node</generator><lastBuildDate>Tue, 12 May 2026 15:15:06 GMT</lastBuildDate><atom:link href="https://cfd-china.com/topic/1045.rss" rel="self" type="application/rss+xml"/><pubDate>Mon, 25 Sep 2017 09:39:37 GMT</pubDate><ttl>60</ttl><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Mon, 15 Mar 2021 08:16:04 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/856">@Ryo</a> 前辈好！  请问Gmesh能够对非结构网格划分block吗?</p>
]]></description><link>https://cfd-china.com/post/24722</link><guid isPermaLink="true">https://cfd-china.com/post/24722</guid><dc:creator><![CDATA[liujunCFD]]></dc:creator><pubDate>Mon, 15 Mar 2021 08:16:04 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Tue, 04 Dec 2018 15:56:01 GMT]]></title><description><![CDATA[<p dir="auto">@东岳<br />
Thanks very much for reply.I totally understand.</p>
<p dir="auto">Please take your own time, reply me just when you are leisure ,I will try my best to solve the problem on myself .</p>
<p dir="auto">really thanks a lot for so long. best wishes !</p>
]]></description><link>https://cfd-china.com/post/10737</link><guid isPermaLink="true">https://cfd-china.com/post/10737</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Tue, 04 Dec 2018 15:56:01 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Tue, 04 Dec 2018 13:42:49 GMT]]></title><description><![CDATA[<p dir="auto">Let me try to complete the mesh this week, I am pretty busy</p>
<p dir="auto">:oooooooooooooo</p>
]]></description><link>https://cfd-china.com/post/10729</link><guid isPermaLink="true">https://cfd-china.com/post/10729</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Tue, 04 Dec 2018 13:42:49 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Sat, 01 Dec 2018 08:29:53 GMT]]></title><description><![CDATA[<p dir="auto">@东岳<br />
多谢老师回复 现在没搞懂这些边是怎么添加上去的 （上面的斜线和右边圆里面的不规则四面体）sorry 刚上手这个软件 。<br />
然后我简化的画了网格 还有之前的问题。。</p>
<p dir="auto"><img src="/assets/uploads/files/1543652646356-555-resized.png" alt="0_1543652645233_555.PNG" class=" img-fluid img-markdown" /></p>
<p dir="auto">这是我画的切的block<img src="/assets/uploads/files/1543652817471-345-resized.png" alt="0_1543652816817_345.PNG" class=" img-fluid img-markdown" /><br />
<img src="/assets/uploads/files/1543652835394-3435-resized.png" alt="0_1543652834568_3435.PNG" class=" img-fluid img-markdown" /></p>
<p dir="auto">这是画的网格<img src="/assets/uploads/files/1543652906273-367-resized.png" alt="0_1543652903764_367.PNG" class=" img-fluid img-markdown" /><br />
sorry 实在是有点太小白了 麻烦老师了。</p>
]]></description><link>https://cfd-china.com/post/10693</link><guid isPermaLink="true">https://cfd-china.com/post/10693</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Sat, 01 Dec 2018 08:29:53 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Sat, 01 Dec 2018 01:22:31 GMT]]></title><description><![CDATA[<p dir="auto"><img src="/assets/uploads/files/1543627325164-%E6%8D%95%E8%8E%B7.jpg" alt="0_1543627323918_捕获.JPG" class=" img-fluid img-markdown" /></p>
<p dir="auto">你按照我这样分block<br />
有点事我要出去</p>
]]></description><link>https://cfd-china.com/post/10685</link><guid isPermaLink="true">https://cfd-china.com/post/10685</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Sat, 01 Dec 2018 01:22:31 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Fri, 30 Nov 2018 06:18:28 GMT]]></title><description><![CDATA[<p dir="auto">@东岳 多谢老师<br />
这是tin文件 传到dropbox上的<br />
<a href="https://www.dropbox.com/s/4zw6pr4f9hvy86v/12345.tin?dl=0" target="_blank" rel="noopener noreferrer nofollow ugc">https://www.dropbox.com/s/4zw6pr4f9hvy86v/12345.tin?dl=0</a><br />
这是prj文件在dropbox上的<br />
<a href="https://www.dropbox.com/s/997ohw1j55uw2z3/12345.prj?dl=0" target="_blank" rel="noopener noreferrer nofollow ugc">https://www.dropbox.com/s/997ohw1j55uw2z3/12345.prj?dl=0</a></p>
<p dir="auto">我用snappyHexMesh弄的网格数在180万左右，网格少点没事，感谢老师啦Thanks♪(･ω･)ﾉ</p>
]]></description><link>https://cfd-china.com/post/10666</link><guid isPermaLink="true">https://cfd-china.com/post/10666</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Fri, 30 Nov 2018 06:18:28 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Fri, 30 Nov 2018 05:21:53 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/856">@Ryo</a></p>
<p dir="auto">你的网格质量很差，导入的时候有可能出现问题。把你的tin文件上传一下我给你画一个</p>
<p dir="auto">这个帖子竟然48楼了 <img src="https://cfd-china.com/assets/plugins/nodebb-plugin-emoji/emoji/customizations/dae37077-ed45-4a9a-994b-5a40d8188193-365e0c1284d7823b844b8a6c43280855.png?v=eedi85amb0g" class="not-responsive emoji emoji-customizations emoji--papa" style="height:23px;width:auto;vertical-align:middle" title=":papa:" alt=":papa:" /></p>
]]></description><link>https://cfd-china.com/post/10665</link><guid isPermaLink="true">https://cfd-china.com/post/10665</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Fri, 30 Nov 2018 05:21:53 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Fri, 30 Nov 2018 05:02:59 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/2294">@regina</a> Hi!</p>
<p dir="auto">openfoam不能直接进入密度场，密度是由其他物理条件（p，u,t...etc）计算出来的，我也想直接设置密度😭。。  我是通过调节初始p,u,t来调节初始的密度。sorry，不知道帮到你了没有。。</p>
<p dir="auto">另外你知道我这网格为啥会有这问题吗？ 然后我把这网格用fluentToFoam了下发现报错<br />
<img src="/assets/uploads/files/1543554088236-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2018-11-30-14.00.50.png" alt="0_1543554083798_屏幕快照 2018-11-30 14.00.50.png" class=" img-fluid img-markdown" /><br />
<img src="/assets/uploads/files/1543554105032-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2018-11-30-14.01.05.png" alt="0_1543554101591_屏幕快照 2018-11-30 14.01.05.png" class=" img-fluid img-markdown" /></p>
<p dir="auto">之前用gmesh这样gmshToFoam都没问题可以转。。</p>
]]></description><link>https://cfd-china.com/post/10664</link><guid isPermaLink="true">https://cfd-china.com/post/10664</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Fri, 30 Nov 2018 05:02:59 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Fri, 30 Nov 2018 03:33:36 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/856">@ryo</a> 不太明白为什么动力粘度就不需要单独设置密度了呢，那如果我需要设置成水的属性，密度为1000kg/m^3，运动粘性系数=1.139×10^-6Pa*s。除了修改属性设置文件transportProperties中的粘度，我怎么保证密度也是我想要的1000kg/m^3呢？希望能指导一二，跪谢</p>
]]></description><link>https://cfd-china.com/post/10661</link><guid isPermaLink="true">https://cfd-china.com/post/10661</guid><dc:creator><![CDATA[Regina]]></dc:creator><pubDate>Fri, 30 Nov 2018 03:33:36 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Thu, 29 Nov 2018 08:54:18 GMT]]></title><description><![CDATA[<p dir="auto">@东岳<br />
又来麻烦老师了。之前用snappyHexMesh做的网格感觉不好现在想换用icem cfd来做，弄了好几天发现喷口旁边座位阻碍物的圆柱的网格有大瑕疵（表面的都很好），找了很多视频里面都没有找到该怎么去掉圆柱里面这些不需要的网格。<br />
另外icem cfd做好的网格怎么导入openfoam和paraview现在也没找出来方法。 请老师给点指示。<br />
<img src="/assets/uploads/files/1543480876065-inked%E6%8D%95%E8%8E%B7_li%E9%A3%9E.jpg" alt="0_1543480873745_Inked捕获_LI飞.jpg" class=" img-fluid img-markdown" /></p>
<p dir="auto"><img src="/assets/uploads/files/1543481637027-3.jpg" alt="0_1543481633906_3.jpg" class=" img-fluid img-markdown" /></p>
<p dir="auto">🙏🙏</p>
]]></description><link>https://cfd-china.com/post/10654</link><guid isPermaLink="true">https://cfd-china.com/post/10654</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Thu, 29 Nov 2018 08:54:18 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Mon, 26 Nov 2018 02:27:45 GMT]]></title><description><![CDATA[<p dir="auto">@东岳<br />
懂了，多谢老师。</p>
]]></description><link>https://cfd-china.com/post/10605</link><guid isPermaLink="true">https://cfd-china.com/post/10605</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Mon, 26 Nov 2018 02:27:45 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Thu, 22 Nov 2018 23:57:44 GMT]]></title><description><![CDATA[<p dir="auto"><img src="/assets/uploads/files/1542931055198-%E6%8D%95%E8%8E%B7.jpg" alt="0_1542931053530_捕获.JPG" class=" img-fluid img-markdown" /></p>
<p dir="auto">你点击一下这个试试</p>
]]></description><link>https://cfd-china.com/post/10568</link><guid isPermaLink="true">https://cfd-china.com/post/10568</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Thu, 22 Nov 2018 23:57:44 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Thu, 22 Nov 2018 07:42:49 GMT]]></title><description><![CDATA[<p dir="auto">@东岳<br />
sorry 😂<br />
先跑一遍rho：把data放到paraview里面选择rho然后点击play<br />
<img src="/assets/uploads/files/1542872177896-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2018-11-22-16.10.30.png" alt="0_1542872176845_屏幕快照 2018-11-22 16.10.30.png" class=" img-fluid img-markdown" /></p>
<p dir="auto">先跑一遍p在调节到rho：把data放到paraview里面先选择p然后点击play在从p调节到rho<br />
<img src="/assets/uploads/files/1542872218591-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2018-11-22-16.09.03.png" alt="0_1542872217819_屏幕快照 2018-11-22 16.09.03.png" class=" img-fluid img-markdown" /></p>
<p dir="auto">想说的意思可能就是第一遍play显示的数据图像和play完第一遍后切换到其他性质（比如从密度切换到压强，压强切换到密度）后在切换回来显示的不一样。一样的data为什么会显示的不一样呢？ 问题解释的可能有点傻，请见谅。。</p>
]]></description><link>https://cfd-china.com/post/10556</link><guid isPermaLink="true">https://cfd-china.com/post/10556</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Thu, 22 Nov 2018 07:42:49 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Wed, 21 Nov 2018 09:04:20 GMT]]></title><description><![CDATA[<p dir="auto">什么是“先跑一遍rho和先跑完一遍p”... <img src="https://cfd-china.com/assets/plugins/nodebb-plugin-emoji/emoji/customizations/3bb52208-0334-4a4f-b00b-10af7f80b44a-6f9587ea79464fd653058d977c355d76.png?v=eedi85amb0g" class="not-responsive emoji emoji-customizations emoji--zoule" style="height:23px;width:auto;vertical-align:middle" title=":zoule:" alt=":zoule:" /> <img src="https://cfd-china.com/assets/plugins/nodebb-plugin-emoji/emoji/customizations/3bb52208-0334-4a4f-b00b-10af7f80b44a-6f9587ea79464fd653058d977c355d76.png?v=eedi85amb0g" class="not-responsive emoji emoji-customizations emoji--zoule" style="height:23px;width:auto;vertical-align:middle" title=":zoule:" alt=":zoule:" /> <img src="https://cfd-china.com/assets/plugins/nodebb-plugin-emoji/emoji/customizations/3bb52208-0334-4a4f-b00b-10af7f80b44a-6f9587ea79464fd653058d977c355d76.png?v=eedi85amb0g" class="not-responsive emoji emoji-customizations emoji--zoule" style="height:23px;width:auto;vertical-align:middle" title=":zoule:" alt=":zoule:" /></p>
]]></description><link>https://cfd-china.com/post/10532</link><guid isPermaLink="true">https://cfd-china.com/post/10532</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Wed, 21 Nov 2018 09:04:20 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Wed, 21 Nov 2018 02:54:54 GMT]]></title><description><![CDATA[<p dir="auto">@东岳  Hi!<br />
又要来麻烦老师了🙏</p>
<p dir="auto">之前的涡的存在问题已经解决。原因是因为压力边界条件设置问题，还有发现k和epsilon之前按照公式算的是10的5次方级别的数字 但是我把他调节成0.5也能算而且精度更准，这个还不知道什么原因。。</p>
<p dir="auto">现在（其实从之前）就有个关于paraview的问题，把data放到paraview里面显示rho跑第一遍的colour legend和先显示p跑一遍在切换到rho显示的colour legend有些许的不同。</p>
<p dir="auto">这是显示rho跑第一遍的图  colour legend只显示到0.23<br />
<img src="/assets/uploads/files/1542768675031-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2018-11-21-11.46.20.png" alt="0_1542768671839_屏幕快照 2018-11-21 11.46.20.png" class=" img-fluid img-markdown" /></p>
<p dir="auto">这是先跑完一遍p在切换到rho， colour legend就可以显示到0.06<br />
<img src="/assets/uploads/files/1542768801542-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2018-11-21-11.46.33.png" alt="0_1542768794615_屏幕快照 2018-11-21 11.46.33.png" class=" img-fluid img-markdown" /></p>
<p dir="auto">求老师给点指示</p>
]]></description><link>https://cfd-china.com/post/10527</link><guid isPermaLink="true">https://cfd-china.com/post/10527</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Wed, 21 Nov 2018 02:54:54 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Thu, 21 Dec 2017 09:09:46 GMT]]></title><description><![CDATA[<pre><code>volScalarField rho
    (
        IOobject
        (
            "rho",
            runTime.timeName(),
            mesh
        ),
        thermo.rho()
    );
</code></pre>
<p dir="auto">OpenFOAM里面的密度是通过<code>thermo.rho()</code>更新的，因此你不能直接给密度。</p>
<blockquote>
<p dir="auto">更改fvscheme后达到预期的冲击波外的区域密度场都1左右，但是发现冲击波前面的涡很微弱。这是实验得到的图像。冲击波前面有很明显的蓝色的涡。</p>
</blockquote>
<p dir="auto">云图看起来不是很客观，最好出<code>plot</code>图看看</p>
]]></description><link>https://cfd-china.com/post/6519</link><guid isPermaLink="true">https://cfd-china.com/post/6519</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Thu, 21 Dec 2017 09:09:46 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Fri, 15 Dec 2017 08:55:14 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/1">@李东岳</a><br />
老师好！发现openfoam是不能直接进入密度场的因为openfoam用的是kinematic viscasity.fluent用的是动力粘度。<br />
<img src="/assets/uploads/files/1513326955985-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-12-14-16.26.35.png" alt="0_1513326954486_屏幕快照 2017-12-14 16.26.35.png" class=" img-fluid img-markdown" /><br />
所以感觉还是得调节p，之前的压力边界条件我设置的是outlet为0.2大气压，inlet为zerogradient。现在调换后inlet为0.2大气压，outlet为zerogradient，initial为1个大气压。然后按照<br />
<img src="/assets/uploads/files/1513327736649-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-12-15-17.46.38.png" alt="0_1513327734658_屏幕快照 2017-12-15 17.46.38.png" class=" img-fluid img-markdown" /><br />
更改fvscheme后达到预期的冲击波外的区域密度场都1左右，但是发现冲击波前面的涡很微弱。<br />
这是实验得到的图像。冲击波前面有很明显的蓝色的涡。<br />
<img src="/assets/uploads/files/1513328034208-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-11-20-13.59.32.png" alt="0_1513328028553_屏幕快照 2017-11-20 13.59.32.png" class=" img-fluid img-markdown" /><br />
这是openfoam得到的图像，冲击波前面基本没有涡<br />
<img src="/assets/uploads/files/1513328100816-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-12-15-17.52.52.png" alt="0_1513328098516_屏幕快照 2017-12-15 17.52.52.png" class=" img-fluid img-markdown" /></p>
]]></description><link>https://cfd-china.com/post/6448</link><guid isPermaLink="true">https://cfd-china.com/post/6448</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Fri, 15 Dec 2017 08:55:14 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Tue, 12 Dec 2017 06:41:59 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/1">@李东岳</a> 感谢老师回复 🙏</p>
<p dir="auto">Mac上还是没有找到什么原因wmake出错，但是在虚拟机（Linux Mint）上在按照openfoam wiki上添加温度的教程编译成功了。<br />
发现 在createfields.H里加Oobject::MUST_READ,IObject::AUTO_WRITE，和在/systym/controlDict里面加<br />
<img src="/assets/uploads/files/1513060712764-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-12-12-15.37.48-resized.png" alt="0_1513060706790_屏幕快照 2017-12-12 15.37.48.png" class=" img-fluid img-markdown" /><br />
效果一样 都只是根据初始p，U，粘度等来计算密度，不能直接读取0文件夹里面的rho文件。。。<br />
这是0文件夹里面的rho文件 虽然设置的是1但是计算后在paraview上显示是0.23<br />
<img src="/assets/uploads/files/1513060819347-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-12-12-15.31.18-resized.png" alt="0_1513060816206_屏幕快照 2017-12-12 15.31.18.png" class=" img-fluid img-markdown" /><br />
怎么才能跟fluent一样直接调节初始场密度呢。<br />
麻烦老师在看下🙏</p>
]]></description><link>https://cfd-china.com/post/6377</link><guid isPermaLink="true">https://cfd-china.com/post/6377</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Tue, 12 Dec 2017 06:41:59 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Sat, 09 Dec 2017 07:53:49 GMT]]></title><description><![CDATA[<p dir="auto">不好意思没有mac不能提供建设性意见 :big_mouth:</p>
]]></description><link>https://cfd-china.com/post/6342</link><guid isPermaLink="true">https://cfd-china.com/post/6342</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Sat, 09 Dec 2017 07:53:49 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Fri, 08 Dec 2017 09:26:39 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/1">@李东岳</a> 谢谢 回复。🙏<br />
Make/option里面本来就有这些码。<img src="/assets/uploads/files/1512725186321-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-12-08-18.23.08-resized.png" alt="0_1512725181546_屏幕快照 2017-12-08 18.23.08.png" class=" img-fluid img-markdown" /></p>
]]></description><link>https://cfd-china.com/post/6336</link><guid isPermaLink="true">https://cfd-china.com/post/6336</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Fri, 08 Dec 2017 09:26:39 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Wed, 06 Dec 2017 11:48:04 GMT]]></title><description><![CDATA[<p dir="auto">在你的<code>Make/option</code>里面添加</p>
<pre><code>//EXE_INC = \下面加
-I$(LIB_SRC)/meshTools/lnInclude \

//EXE_LIBS = \下面加
-lmeshTools \
</code></pre>
<p dir="auto">试试</p>
]]></description><link>https://cfd-china.com/post/6312</link><guid isPermaLink="true">https://cfd-china.com/post/6312</guid><dc:creator><![CDATA[李东岳]]></dc:creator><pubDate>Wed, 06 Dec 2017 11:48:04 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Wed, 06 Dec 2017 09:30:54 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/856">@ryo</a> 不是wmke是 wmake，刚才手误</p>
]]></description><link>https://cfd-china.com/post/6311</link><guid isPermaLink="true">https://cfd-china.com/post/6311</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Wed, 06 Dec 2017 09:30:54 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Wed, 06 Dec 2017 09:29:39 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/1">@李东岳</a> 李老师，现在想重新编译时按照http://openfoamwiki.net/index.php/How_to_add_temperature_to_icoFoam。 这个教程想练一遍，发现wmake的时候出现错误</p>
<pre><code>/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::STARCDCore::STARCDCore()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::fileName const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::STARCDCore::starFileName(Foam::fileName const&amp;, Foam::fileFormats::STARCDCore::fileExt)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `typeinfo for Foam::OBJstream'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::vtk::legacy::contentNames'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::reduce(Foam::Vector2D&lt;double&gt;&amp;, Foam::sumOp&lt;Foam::Vector2D&lt;double&gt; &gt; const&amp;, int, int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::OBJstream::~OBJstream()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::freePstreamCommunicator(int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::geometricSurfacePatch::geometricSurfacePatch(Foam::word const&amp;, int, Foam::word const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::UPstream::finishedRequest(int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::scalePoints(double)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::xferPoints()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::DimensionedField&lt;double, Foam::triSurfacePointGeoMesh&gt;::typeName'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::STARCDCore::writePoints(Foam::Ostream&amp;, Foam::Field&lt;Foam::Vector&lt;double&gt; &gt; const&amp;, double)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::xferFaces()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::OBJstream::write(Foam::Vector&lt;double&gt; const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::NASCore::parseNASCoord(Foam::string const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::fileName const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::STARCDCore::writeHeader(Foam::Ostream&amp;, Foam::fileFormats::STARCDCore::fileHeader)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::abort()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::vtk::legacy::fileHeader(Foam::vtk::formatter&amp;, std::string const&amp;, std::string const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::DimensionedField&lt;double, Foam::triSurfaceGeoMesh&gt;::typeName'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::subsetMesh(Foam::List&lt;bool&gt; const&amp;, Foam::List&lt;int&gt;&amp;, Foam::List&lt;int&gt;&amp;) const'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::OBJstream::write(Foam::face const&amp;, Foam::UList&lt;Foam::Vector&lt;double&gt; &gt; const&amp;, bool)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::vtk::outputOptions::legacy(bool)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::canRead(Foam::fileName const&amp;, bool)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::STARCDCore::readPoints(Foam::IFstream&amp;, Foam::Field&lt;Foam::Vector&lt;double&gt; &gt;&amp;, Foam::List&lt;int&gt;&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::resetRequests(int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::allocatePstreamCommunicator(int, int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::edgeOwner() const'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::OBJstream::OBJstream(Foam::fileName const&amp;, Foam::IOstream::streamFormat, Foam::IOstream::versionNumber, Foam::IOstream::compressionType)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::OBJstream::write(Foam::UList&lt;Foam::face&gt; const&amp;, Foam::Field&lt;Foam::Vector&lt;double&gt; &gt; const&amp;, bool)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::List&lt;Foam::labelledTri&gt; const&amp;, Foam::List&lt;Foam::geometricSurfacePatch&gt; const&amp;, Foam::Field&lt;Foam::Vector&lt;double&gt; &gt; const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::init(int&amp;, char**&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::geometricSurfacePatch::geometricSurfacePatch()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::UPstream::allToAll(Foam::UList&lt;int&gt; const&amp;, Foam::UList&lt;int&gt;&amp;, int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::STARCDCore::readHeader(Foam::IFstream&amp;, Foam::fileFormats::STARCDCore::fileHeader)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::UIPstream::UIPstream(int, Foam::PstreamBuffers&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::~triSurface()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UIPstream::UIPstream(Foam::UPstream::commsTypes, int, Foam::DynamicList&lt;char, 0u, 2u, 1u&gt;&amp;, int&amp;, int, int, bool, Foam::IOstream::streamFormat, Foam::IOstream::versionNumber)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::sumReduce(double&amp;, int&amp;, int, int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::reduce(double&amp;, Foam::minOp&lt;double&gt; const&amp;, int, int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::operator=(Foam::triSurface const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `typeinfo for Foam::vtk::formatter'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::sortedEdgeFaces() const'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::vtk::legacy::dataTypeNames'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::coordSet::coordSet(Foam::word const&amp;, Foam::word const&amp;, Foam::List&lt;Foam::Vector&lt;double&gt; &gt; const&amp;, Foam::List&lt;double&gt; const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::List&lt;Foam::labelledTri&gt; const&amp;, Foam::Field&lt;Foam::Vector&lt;double&gt; &gt; const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::triSurface const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::List&lt;Foam::labelledTri&gt;&amp;, Foam::List&lt;Foam::geometricSurfacePatch&gt; const&amp;, Foam::Field&lt;Foam::Vector&lt;double&gt; &gt;&amp;, bool)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::addValidParOptions(Foam::HashTable&lt;Foam::string, Foam::word, Foam::string::hash&gt;&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so: undefined reference to `Foam::UPstream::exit(int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::vtk::newFormatter(std::ostream&amp;, Foam::vtk::formatType, unsigned int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::vtkUnstructuredReader::vtkUnstructuredReader(Foam::objectRegistry const&amp;, Foam::ISstream&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::operator==(Foam::geometricSurfacePatch const&amp;, Foam::geometricSurfacePatch const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::~triSurface()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libfiniteVolume.so: undefined reference to `Foam::UPstream::waitRequest(int)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::OBJstream::write(Foam::UList&lt;Foam::edge&gt; const&amp;, Foam::UList&lt;Foam::Vector&lt;double&gt; &gt; const&amp;, bool)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::write(Foam::fileName const&amp;, bool) const'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `typeinfo for Foam::triSurface'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::movePoints(Foam::Field&lt;Foam::Vector&lt;double&gt; &gt; const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::DimensionedField&lt;int, Foam::triSurfaceGeoMesh&gt;::typeName'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::triSurface(Foam::triSurface const&amp;)'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::markZones(Foam::List&lt;bool&gt; const&amp;, Foam::List&lt;int&gt;&amp;) const'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::fileFormats::NASCore::NASCore()'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::writeStats(Foam::Ostream&amp;) const'
/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/lib/libmeshTools.so: undefined reference to `Foam::triSurface::clearOut()'
collect2: error: ld returned 1 exit status
make: *** [/opt/OpenFOAM/OpenFOAM-v1706/platforms/linux64GccDPInt32Opt/bin/my_icoFoam] Error 1
sh-4.2# 
</code></pre>
<p dir="auto">我在想是不是用mac的原因于是 我又在虚拟机上（linux mint）上试了下，直接告诉我wmke command can not found<br />
。。不知道时怎搞的了。。能帮忙看下哪里出错了吗。<br />
🙏</p>
]]></description><link>https://cfd-china.com/post/6310</link><guid isPermaLink="true">https://cfd-china.com/post/6310</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Wed, 06 Dec 2017 09:29:39 GMT</pubDate></item><item><title><![CDATA[Reply to 新手求问冲击波管喷出的低马赫数supersonic的 边界条件问题 on Mon, 27 Nov 2017 08:48:27 GMT]]></title><description><![CDATA[<p dir="auto"><a class="plugin-mentions-user plugin-mentions-a" href="https://cfd-china.com/uid/1">@李东岳</a><br />
感谢回复🙏</p>
<p dir="auto">现在所在的这个研究室在做用独创的激光CT法观测从冲击波管里面喷出的冲击波密度场。 所以我现在想用OpenFOAM作为CFD工具模拟出冲击波的密度场，然后再和真实实验中的图像数据做对比。<br />
sonicfoam里面计算出的结果没发显示密度，在网上找了个代表密度函数的代码放到controldict里面后可以显示密度了但是不能直接在0文件夹里面调节初始密度场。<br />
这是放在controlDict里面的代码<br />
<img src="/assets/uploads/files/1511771946888-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-11-27-17.14.32-resized.png" alt="0_1511771945812_屏幕快照 2017-11-27 17.14.32.png" class=" img-fluid img-markdown" /></p>
<p dir="auto">现在把Oobject::MUST_READ,IObject::AUTO_WRITE加到createFields.H里面后，计算时仍然不读取0文件夹里面的密度边界条件和初始密度场。。<br />
<img src="/assets/uploads/files/1511772209353-%E5%B1%8F%E5%B9%95%E5%BF%AB%E7%85%A7-2017-11-27-16.24.51-resized.jpg" alt="0_1511772192335_屏幕快照 2017-11-27 16.24.51.jpg" class=" img-fluid img-markdown" /></p>
<p dir="auto">想问还需要编译什么才能直接调节初始场的密度。<br />
麻烦老师啦🙏</p>
]]></description><link>https://cfd-china.com/post/6182</link><guid isPermaLink="true">https://cfd-china.com/post/6182</guid><dc:creator><![CDATA[Ryo]]></dc:creator><pubDate>Mon, 27 Nov 2017 08:48:27 GMT</pubDate></item></channel></rss>