algorithmic modeling for Rhino

Search Results - 2017年12月5号双色球-『2TBH·COM』-大乐透13071期死若夏花预测--2023年3月24日19时42分29秒.H5c2a3.kddvkeino.com

Topic: Mode shape animation in GH: actually can perform using a dedicated software: in 3D: https://www.facebook.com/francescopiasentini/videos/523532707845171/ in 2D: https://vimeo.com/189618609 The output of Modal Analysis (at a given frequency) is a list of point (x,y,z), each of them has the three coordinates and the maximum displacement in the direction normal to the surface (that's not flat) Point number x y zmax1 24,007565 337,876028 -0,6545572 -28,0404705 337,947773 0,7760153 57,141457 316,757768 -0,8413914 18,667466 314,814543 -0,235288 My idea is: -import stl surfaces of the object (violin) -import Modal Analysis data -deform stl (or Nurbs) surfaces using something like a customized CageEdit -animate this deformation from zero to maximum displacement -give a color to deformation (or first-second derivative of the interpoled deformation curves) My wish is to have closed surfaces at any steps, and to create "natural" deformation shapes. I just tried to import MA data. I was trying to create an array of circles with given x,y,z and radius, I could not figure how to separate information of position and radius when importing the file: file content: 0,1,0; 5;2,1,3; 2;5,2,6; 4; thanks for yout attention. Looking forward to hear you soon! Francesco …; Added by piase at 2:10am on May 31, 2017

Topic: Nested arrays/lists to datatrees: to convert nested arrays ? For intance if I have 5 times nested array, do I need to another method, or there is a short quick version that combines all three methods below into 1? public static DataTree<T> IEOfIEToTree<T>(IEnumerable<IEnumerable<T>> list, int iteration = 0) { DataTree<T> tree = new DataTree<T>(); int i = 0; foreach (IEnumerable<T> innerList in list) { tree.AddRange(innerList, new GH_Path(new int[] { iteration, i })); i++; } return tree; } public static DataTree<T> IE3<T>(IEnumerable<IEnumerable<IEnumerable<T>>> list, int iteration = 0) { DataTree<T> tree = new DataTree<T>(); int i = 0; foreach (IEnumerable<IEnumerable<T>> innerList in list) { int j = 0; foreach (IEnumerable<T> innerList2 in innerList) { tree.AddRange(innerList2, new GH_Path(new int[] { iteration, i, j })); j++; } i++; } return tree; } public static DataTree<T> IE4<T>(IEnumerable<IEnumerable<IEnumerable<IEnumerable<T>>>> list, int iteration = 0) { DataTree<T> tree = new DataTree<T>(); int i = 0; foreach (IEnumerable<IEnumerable<IEnumerable<T>>> innerList in list) { int j = 0; foreach (IEnumerable<IEnumerable<T>> innerList2 in innerList) { int k = 0; foreach (IEnumerable<T> innerList3 in innerList2) { tree.AddRange(innerList3, new GH_Path(new int[] { iteration, i, j ,k})); k++; } j++; } i++; } return tree; }…; Added by Petras Vestartas at 11:24am on October 17, 2017

Topic: Few notes to celebrate two years and two weeks of having the 'bug flying around!: and I here is what I have to share: Thanks! Thank you for being awesome! When I released Ladybug two years ago I could never imagine how this project will take over my life! It has been such an invaluable experience for me so far and it wasn’t possible without you - so thank you so much. What’s next? Recently I get this question more and more and here is my fairly long answer! Chris is pushing the boundaries with comfort tools. Chien Si is working on HVAC systems integration. Chris, Anton and Alejandra will figure out how to effectively get natural ventilation to be modeled. Patrick, Sandeep, Michal and Boris are working on their developments. I’m working on getting 3 Phase method integrated, and Butterfly will be out at some point, but... they are not going to be what makes the next step. The next step is up to you. It is what you will do with the development. So go ahead and let us know what’s next! If you can help someone on the group please do! Doing so you are not only helping another person (and potentially yourself) but also the developers. The more you can help each other here the more we will have time for development and documentation. Best place to send your questions is this group. If you are using the latest version from github then you may want to sent it to github. Please consider emails as the last option. Go back to number 3 again! Thanks. Don’t be nice to us! Well, I mean don’t just be nice to us. I love your nice comments like anybody else and please keep them coming ;) but what we also need next to nice comments is your critiques, wishes and insight. I feel that recently we are getting less wishes and critiques than what it used to be. You can post them here in the group or on github and either way we will know about it. Thank you to all of you who has already done this. Thanks again! Before I let you go I want to specially thank all of you who contributed to the project by your development, thoughts and support. You are great and I can’t thank you enough. David Weinberger in his book “Too Big to Know” says: “When an expert network is functioning as its best, the smartest person in the room is the room itself.” Reading some of the discussions on the group gives me the feeling of staying inside a smart room. Thank you and let’s keep the room growing! Cheers, Mostapha PS: To avoid sending another post, I just post the updates about the two upcoming workshops here: I will lead a workshop in LA next Friday (Feb. 6) and there is still few seats left. If you want to learn more about energy and daylighting simulation with Honeybee here is your chance. Here is more information who to register: (http://www.facadesplus.com/technology-workshops/). Chris will lead a 3 days intense and comprehensive Ladybug and Honeybee workshop in Mexico City this March. You have probably watched Chris’s tutorials and already know what you can expect from a workshop with Chris so I don’t have to speak for that! I would take this workshop if I was around that area. If you are around Mexico City or know a friend who might be interested please let them know. Here is more information about the workshop: (https://www.facebook.com/LadyBugforGrasshopper/photos/a.442320969114095.107084.413910668621792/919318878080966). …; Added by Mostapha Sadeghipour Roudsari to Ladybug Tools at 10:00am on January 26, 2015

Topic: Maximum arguments reached for this object, trying to process: 8.3.0 ************* IDF Context for following error/warning message: ************* Note -- lines truncated at 300 characters, if necessary... ************* 829 Construction, ************* indicated Name=PELLE001 ************* Only last 10 lines before error line shown..... ************* 832 AIR WALL2, !- - Layer 2 ************* 833 X-LAM, !- - Layer 3 ************* 834 POLYSTYRENE2, !- - Layer 4 ************* 835 PANNELLO VIP, !- - Layer 5 ************* 836 POLYSTYRENE2, !- - Layer 6 ************* 837 X-LAM, !- - Layer 7 ************* 838 LANA DI ROCCIAS, !- - Layer 8 ************* 839 VANO IMPIANTI, !- - Layer 9 ************* 840 LANA DI ROCCIAS, !- - Layer 10 ************* 841 LASTRA IN GESSOFIBRA, !- - Layer 11 ** Severe ** IP: IDF line~841 Error detected for Object=CONSTRUCTION ** ~~~ ** Maximum arguments reached for this object, trying to process ->LASTRA IN GESSOFIBRA<- ************* IDF Context for following error/warning message: ************* Note -- lines truncated at 300 characters, if necessary... ************* 985 Construction, ************* indicated Name=ROOF001 ************* Only last 10 lines before error line shown..... ************* 988 TRAVETTI, !- - Layer 2 ************* 989 TAVOLATO, !- - Layer 3 ************* 990 POLYSTYRENE2, !- - Layer 4 ************* 991 PANNELLO VIP, !- - Layer 5 ************* 992 POLYSTYRENE2, !- - Layer 6 ************* 993 X-LAM, !- - Layer 7 ************* 994 LANA DI ROCCIAS, !- - Layer 8 ************* 995 VANO IMPIANTI, !- - Layer 9 ************* 996 LANA DI ROCCIAS, !- - Layer 10 ************* 997 LASTRA IN GESSOFIBRA, !- - Layer 11 ** Severe ** IP: IDF line~997 Error detected for Object=CONSTRUCTION ** ~~~ ** Maximum arguments reached for this object, trying to process ->LASTRA IN GESSOFIBRA<- ** Warning ** IP: Note -- Some missing fields have been filled with defaults. See the audit output file for details. ** Severe ** IP: Possible incorrect IDD File ** ~~~ ** IDD Version:"IDD_Version 8.3.0" ** ~~~ ** Version in IDF="8.3" not the same as expected="8.3" ** ~~~ ** Possible Invalid Numerics or other problems ** Fatal ** IP: Errors occurred on processing IDF file. Preceding condition(s) cause termination. ...Summary of Errors that led to program termination: ..... Reference severe error count=3 ..... Last severe error=IP: Possible incorrect IDD File ************* Warning: Node connection errors not checked - most system input has not been read (see previous warning). ************* Fatal error -- final processing. Program exited before simulations began. See previous error messages. ************* EnergyPlus Warmup Error Summary. During Warmup: 0 Warning; 0 Severe Errors. ************* EnergyPlus Sizing Error Summary. During Sizing: 0 Warning; 0 Severe Errors. ************* EnergyPlus Terminated--Fatal Error Detected. 1 Warning; 3 Severe Errors; Elapsed Time=00hr 00min 0.34sec My question is how i can fix it ??? and why it tell me that: ** Severe ** IP: Possible incorrect IDD File** ~~~ ** IDD Version:"IDD_Version 8.3.0"** ~~~ ** Version in IDF="8.3" not the same as expected="8.3"** ~~~ ** Possible Invalid Numerics or other problems** Fatal ** IP: Errors occurred on processing IDF file. Preceding condition(s) cause termination....Summary of Errors that led to program termination: Help me pleaseeeeeeee Happy new year!!!!!…; Added by LHOR at 4:55am on December 31, 2015

Topic: Maximum arguments reached for this object, trying to process: 8.3.0************* IDF Context for following error/warning message:************* Note -- lines truncated at 300 characters, if necessary...************* 829 Construction,************* indicated Name=PELLE001************* Only last 10 lines before error line shown..... ************* 832 AIR WALL2, !- - Layer 2************* 833 X-LAM, !- - Layer 3************* 834 POLYSTYRENE2, !- - Layer 4************* 835 PANNELLO VIP, !- - Layer 5************* 836 POLYSTYRENE2, !- - Layer 6************* 837 X-LAM, !- - Layer 7************* 838 LANA DI ROCCIAS, !- - Layer 8************* 839 VANO IMPIANTI, !- - Layer 9************* 840 LANA DI ROCCIAS, !- - Layer 10************* 841 LASTRA IN GESSOFIBRA, !- - Layer 11** Severe ** IP: IDF line~841 Error detected for Object=CONSTRUCTION** ~~~ ** Maximum arguments reached for this object, trying to process ->LASTRA IN GESSOFIBRA<-************* IDF Context for following error/warning message:************* Note -- lines truncated at 300 characters, if necessary...************* 985 Construction,************* indicated Name=ROOF001************* Only last 10 lines before error line shown.....************* 988 TRAVETTI, !- - Layer 2************* 989 TAVOLATO, !- - Layer 3************* 990 POLYSTYRENE2, !- - Layer 4************* 991 PANNELLO VIP, !- - Layer 5************* 992 POLYSTYRENE2, !- - Layer 6************* 993 X-LAM, !- - Layer 7************* 994 LANA DI ROCCIAS, !- - Layer 8************* 995 VANO IMPIANTI, !- - Layer 9************* 996 LANA DI ROCCIAS, !- - Layer 10************* 997 LASTRA IN GESSOFIBRA, !- - Layer 11** Severe ** IP: IDF line~997 Error detected for Object=CONSTRUCTION** ~~~ ** Maximum arguments reached for this object, trying to process ->LASTRA IN GESSOFIBRA<-** Warning ** IP: Note -- Some missing fields have been filled with defaults. See the audit output file for details.** Severe ** IP: Possible incorrect IDD File** ~~~ ** IDD Version:"IDD_Version 8.3.0"** ~~~ ** Version in IDF="8.3" not the same as expected="8.3"** ~~~ ** Possible Invalid Numerics or other problems** Fatal ** IP: Errors occurred on processing IDF file. Preceding condition(s) cause termination....Summary of Errors that led to program termination:..... Reference severe error count=3..... Last severe error=IP: Possible incorrect IDD File************* Warning: Node connection errors not checked - most system input has not been read (see previous warning).************* Fatal error -- final processing. Program exited before simulations began. See previous error messages.************* EnergyPlus Warmup Error Summary. During Warmup: 0 Warning; 0 Severe Errors.************* EnergyPlus Sizing Error Summary. During Sizing: 0 Warning; 0 Severe Errors.************* EnergyPlus Terminated--Fatal Error Detected. 1 Warning; 3 Severe Errors; Elapsed Time=00hr 00min 0.34sec My question is how i can fix it ??? and why it tell me that: ** Severe ** IP: Possible incorrect IDD File** ~~~ ** IDD Version:"IDD_Version 8.3.0"** ~~~ ** Version in IDF="8.3" not the same as expected="8.3"** ~~~ ** Possible Invalid Numerics or other problems** Fatal ** IP: Errors occurred on processing IDF file. Preceding condition(s) cause termination....Summary of Errors that led to program termination: Help me pleaseeeeeeee Thanks and Happy new year!!!!!…; Added by LHOR to Ladybug Tools at 2:08am on January 1, 2016

Event: computational design: parametric design & digital fabrication: the use of digital technologies as architectural design tools. The workshop " Computer Aided Design: parametric design and digital fabrication " aims to do some introductory teaching in the use of some of these tools. The workshop will focus on the use of computational models of parametric behavior for generating architectural forms. The generative capacity of these models it will be tested in the development of designs defined by repetitive non-standard components, based on the parametric control of its variations and series differentiations. This process will be developed by the use of a three-dimensional modeling software - Rhinoceros, associated with an application for visual programming - Grasshopper. The last day of the workshop is dedicated to the use of digital manufacturing tools in architecture. Part of the work will take place at the facilities of the Institute of Design of Guimarães (IDEGUI) providing for the use of their laboratories and manufacturing CNC machines (computer numerically controlled). At the end of the workshop, it is intended the students to understand that the use of digital technologies in architecture can overcome representational functions, and their integration in the design conception, analysis and construction enriches the methodology of project development. Terms & Participants The workshop will take place at the School of Architecture of the University of Minho (Campus Azurém, Guimarães) and the Institute of Design of Guimarães (Couros, Guimarães). The workshop is pointed at students who attend the 3rd year and 4th year from MiArq, EAUM. The maximum acceptance is 20 students and a minimum of 10 students. Deadline for entries is April 11 and must be performed by eaum.pac@gmail.com. Program summary : Day 23 April 14 -20h Introduction to 3D modeling in Rhinoceros. Regular geometries, ruled surfaces and NURBS surfaces. Day 30 April 14 -20h Parametric design in architecture. Introduction to methods of visual programming. May 1, 9 -13h 14 -18h Development of a design idea by the use visual programming processes in Grasshopper. May 2, 9 -13h 14 -18h Introduction to methods of digital fabrication. Manufacture physical models of the proposals made. It is expected that this meeting will take place in the IDEGUI labs. team: Bruno Figueiredo ( Lecturer, EAUM ) Paulo Sousa ( PhD candidate , EAUM ) Nuno Cruz ( Invited Lecturer , EAUM ) Cláudia Alvares ( 5th year MiArq student , EAUM ) Javier Bono ( 4th year MiArq student, EAUM ) João Amaro ( 5th year MiArq student, EAUM )…; Added by Bruno at 12:20pm on April 2, 2014

Topic: split building mass component error: rce=activity Basically, I want to create a workflow to automatically subdivide a building mass envelope geometry into different floors which will be further subdivided as perimeter zones and core zones. But I encountered an error for a particular building mass geometry (a quite regular form) which doesn't work with the split building mass component (see item 4&5 below): The workflow is: 1. import building mass geometry: 2. divide the building mass into floors (one zone per floor) using one of the two different methods depending on whether the floor surface has holes or not: 3. use the split building mass component to further divide the zone for each floor into perimeter zones and core zone: 4. I tested several building forms which work for this workflow as shown below, except for one form C05 which is a courtyard block with small tower blocks on top of it: 5. in the last step, there is an error from the split building mass component saying that "solution exception: index out of range: 0" ... So, I wonder if this is error is related to the split building mass component or related to the way the building mass geometry is created. Appreciate your kind advice! Thank you!…; Added by Grasshope to Ladybug Tools at 2:24am on March 28, 2016

Topic: Butterfly/Openfoam floating issue: Mark/*---------------------------------------------------------------------------*\| ========= | || \\ / F ield | OpenFOAM: The Open Source CFD Toolbox || \\ / O peration | Version: v1612+ || \\ / A nd | Web: www.OpenFOAM.com || \\/ M anipulation | |\*---------------------------------------------------------------------------*/Build : v1612+Exec : buoyantBoussinesqSimpleFoam -parallelDate : May 22 2017Time : 10:18:58Host : "default"PID : 2839Case : /home/ofuser/workingDir/butterfly/simple_hvacnProcs : 4Slaves : 3("default.2840""default.2841""default.2842")Pstream initialized with:floatTransfer : 0nProcsSimpleSum : 0commsType : nonBlockingpolling iterations : 0sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE).fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 10)allowSystemOperations : Allowing user-supplied system call operations// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //Create timeCreate mesh for time = 0SIMPLE: convergence criteriafield nut tolerance 0.0001field p_rgh tolerance 0.0001field k tolerance 0.0001field U tolerance 0.0001field T tolerance 0.0001field epsilon tolerance 0.0001field alphat tolerance 0.0001Reading thermophysical propertiesReading field TReading field p_rghReading field UReading/calculating face flux field phiSelecting incompressible transport model NewtonianCreating turbulence modelSelecting turbulence model type RASSelecting RAS turbulence model RNGkEpsilonRNGkEpsilonCoeffs{Cmu 0.0845;C1 1.42;C2 1.68;C3 -0.33;sigmak 0.71942;sigmaEps 0.71942;eta0 4.38;beta 0.012;}Reading field alphatReading gReading hRefCalculating field g.hNo MRF models presentRadiation model not active: radiationProperties not foundSelecting radiationModel noneNo finite volume options presentStarting time loopTime = 1smoothSolver: Solving for Ux, Initial residual = 1, Final residual = 0.06427477, No Iterations 4smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 0.06226344, No Iterations 4smoothSolver: Solving for Uz, Initial residual = 1, Final residual = 0.03950103, No Iterations 3smoothSolver: Solving for T, Initial residual = 1, Final residual = 0.03671111, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 0.008356878, No Iterations 86DICPCG: Solving for p_rgh, Initial residual = 0.07888434, Final residual = 0.0006831407, No Iterations 9DICPCG: Solving for p_rgh, Initial residual = 0.007053905, Final residual = 6.211827e-05, No Iterations 71time step continuity errors : sum local = 3777.266, global = 3.22967, cumulative = 3.22967smoothSolver: Solving for epsilon, Initial residual = 0.9994728, Final residual = 0.0532353, No Iterations 4smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.05640973, No Iterations 4ExecutionTime = 2.65 s ClockTime = 3 sTime = 2smoothSolver: Solving for Ux, Initial residual = 0.5142984, Final residual = 0.02186577, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.5242573, Final residual = 0.02244622, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.5106874, Final residual = 0.02933279, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.3832824, Final residual = 0.01046751, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.9825413, Final residual = 0.009757923, No Iterations 799DICPCG: Solving for p_rgh, Initial residual = 0.04390194, Final residual = 0.000303611, No Iterations 9DICPCG: Solving for p_rgh, Initial residual = 0.0073043, Final residual = 7.259574e-05, No Iterations 45time step continuity errors : sum local = 1883567, global = 2227.205, cumulative = 2230.435smoothSolver: Solving for epsilon, Initial residual = 0.08647006, Final residual = 0.000113174, No Iterations 1smoothSolver: Solving for k, Initial residual = 0.1579946, Final residual = 0.01115579, No Iterations 2ExecutionTime = 9.56 s ClockTime = 10 sTime = 3smoothSolver: Solving for Ux, Initial residual = 0.8070853, Final residual = 0.07865708, No Iterations 3smoothSolver: Solving for Uy, Initial residual = 0.8145663, Final residual = 0.03882168, No Iterations 4smoothSolver: Solving for Uz, Initial residual = 0.5761609, Final residual = 0.0390739, No Iterations 4smoothSolver: Solving for T, Initial residual = 0.1644957, Final residual = 0.006771158, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.7802636, Final residual = 0.006709539, No Iterations 13DICPCG: Solving for p_rgh, Initial residual = 0.04575494, Final residual = 0.0004415382, No Iterations 130DICPCG: Solving for p_rgh, Initial residual = 0.005830491, Final residual = 5.648426e-05, No Iterations 78time step continuity errors : sum local = 6.68889e+12, global = -4.053656e+11, cumulative = -4.053656e+11smoothSolver: Solving for epsilon, Initial residual = 1, Final residual = 0.08337707, No Iterations 1smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.08762031, No Iterations 2ExecutionTime = 11.24 s ClockTime = 11 sTime = 4smoothSolver: Solving for Ux, Initial residual = 0.1870785, Final residual = 0.008250987, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.1039591, Final residual = 0.003633928, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.003344756, Final residual = 0.0001428352, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.0360337, Final residual = 0.0008781286, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.9999995, Final residual = 0.7505781, No Iterations 1001DICPCG: Solving for p_rgh, Initial residual = 2.097918e-11, Final residual = 2.097918e-11, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 2.097918e-11, Final residual = 2.097918e-11, No Iterations 0time step continuity errors : sum local = 9.100777e+16, global = -1.152626e+15, cumulative = -1.153031e+15smoothSolver: Solving for epsilon, Initial residual = 0.006323925, Final residual = 0.0002800085, No Iterations 1smoothSolver: Solving for k, Initial residual = 0.9999998, Final residual = 0.08579136, No Iterations 4ExecutionTime = 15.48 s ClockTime = 16 sTime = 5smoothSolver: Solving for Ux, Initial residual = 0.6268107, Final residual = 0.01889084, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.5691313, Final residual = 0.02593386, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.525286, Final residual = 0.01999095, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.1776883, Final residual = 0.004896742, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.8409992, Final residual = 0.008296552, No Iterations 25DICPCG: Solving for p_rgh, Initial residual = 8.57445e-13, Final residual = 8.57445e-13, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 8.57445e-13, Final residual = 8.57445e-13, No Iterations 0time step continuity errors : sum local = 3.230307e+23, global = -5.044393e+14, cumulative = -1.657471e+15smoothSolver: Solving for epsilon, Initial residual = 4.732135e-05, Final residual = 1.311093e-10, No Iterations 1bounding epsilon, min: -1.103807e+26 max: 1.972571e+51 average: 2.670218e+47smoothSolver: Solving for k, Initial residual = 0.04771126, Final residual = 0.002285774, No Iterations 2ExecutionTime = 16.44 s ClockTime = 17 sTime = 6smoothSolver: Solving for Ux, Initial residual = 0.9995642, Final residual = 0.04432588, No Iterations 4smoothSolver: Solving for Uy, Initial residual = 0.9996968, Final residual = 0.04761556, No Iterations 4smoothSolver: Solving for Uz, Initial residual = 0.9858131, Final residual = 0.06924769, No Iterations 3smoothSolver: Solving for T, Initial residual = 0.01200576, Final residual = 0.0002952721, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.9446084, Final residual = 0.005339222, No Iterations 6DICPCG: Solving for p_rgh, Initial residual = 0.08971123, Final residual = 0.0008218812, No Iterations 6DICPCG: Solving for p_rgh, Initial residual = 0.02323654, Final residual = 0.0002319251, No Iterations 193time step continuity errors : sum local = 4.926861e+44, global = -1.110593e+37, cumulative = -1.110593e+37smoothSolver: Solving for epsilon, Initial residual = 1, Final residual = 0.002671469, No Iterations 2bounding epsilon, min: -2.219668e+47 max: 1.75779e+78 average: 3.182358e+73smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.0501481, No Iterations 2bounding k, min: -3.660183e+25 max: 9.966186e+62 average: 8.53815e+58ExecutionTime = 18.1 s ClockTime = 18 sTime = 7smoothSolver: Solving for Ux, Initial residual = 8.069155e-09, Final residual = 8.069155e-09, No Iterations 0smoothSolver: Solving for Uy, Initial residual = 5.382338e-08, Final residual = 7.473481e-09, No Iterations 1smoothSolver: Solving for Uz, Initial residual = 2.092083e-08, Final residual = 2.077615e-09, No Iterations 1smoothSolver: Solving for T, Initial residual = 0.1619372, Final residual = 0.003564584, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 46631.37, No Iterations 1001DICPCG: Solving for p_rgh, Initial residual = 1.64537e-26, Final residual = 1.64537e-26, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 1.64537e-26, Final residual = 1.64537e-26, No Iterations 0time step continuity errors : sum local = 1.468529e+53, global = 5.868436e+40, cumulative = 5.867326e+40smoothSolver: Solving for epsilon, Initial residual = 0.07343377, Final residual = 2.828068e-19, No Iterations 1bounding epsilon, min: -2.257804e+66 max: 8.093947e+109 average: 1.184346e+105smoothSolver: Solving for k, Initial residual = 0.5212037, Final residual = 0.02939162, No Iterations 2ExecutionTime = 22.26 s ClockTime = 22 sTime = 8smoothSolver: Solving for Ux, Initial residual = 0.6924604, Final residual = 0.01784756, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.3637153, Final residual = 0.005737122, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.2793264, Final residual = 0.00626238, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.07790577, Final residual = 0.002676894, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.8911507, Final residual = 0.008688155, No Iterations 18DICPCG: Solving for p_rgh, Initial residual = 1.957294e-52, Final residual = 1.957294e-52, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 1.957294e-52, Final residual = 1.957294e-52, No Iterations 0time step continuity errors : sum local = 8.548233e+90, global = -3.056251e+75, cumulative = -3.056251e+75--------------------------------------------------------------------------mpirun noticed that process rank 1 with PID 2840 on node default exited on signal 8 (Floating point exception).--------------------------------------------------------------------------[1] #0 Foam::error:rintStack(Foam::Ostream&)[0] #0 Foam::error:rintStack(Foam::Ostream&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[0] #1 Foam::sigFpe::sigHandler(int) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[1] #1 Foam::sigFpe::sigHandler(int) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[0] #2 ? in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[1] #2 ? in "/lib64/libc.so.6"[0] #3 Foam::multiply(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) in "/lib64/libc.so.6"[1] #3 Foam::multiply(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[0] #4 Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > Foam:perator*<Foam::fvPatchField, Foam::volMesh>(Foam::tmp<Foam::GeometricField<doub le, Foam::fvPatchField, Foam::volMesh> > const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[1] #4 void Foam::multiply<Foam::fvPatchField, Foam::volMesh>(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so"[1] #5 Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > Foam:perator*<Foam::fvPatchField, Foam::volMesh>(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so"[1] #6 Foam::RASModels::RNGkEpsilon<Foam::IncompressibleT urbulenceModel<Foam::transportModel> >::correct() in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so"[1] #7 ? in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/bin/buoyantBoussinesqSimpleFoam"[1] #8 __libc_start_main in "/lib64/libc.so.6"[1] #9 ? in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/bin/buoyantBoussinesqSimpleFoam"[default:02840] *** Process received signal ***[default:02840] Signal: Floating point exception (8)[default:02840] Signal code: (-6)[default:02840] Failing at address: 0x1f400000b18[default:02840] [ 0] /lib64/libc.so.6(+0x32660)[0x7f516d4f4660][default:02840] [ 1] /lib64/libc.so.6(gsignal+0x35)[0x7f516d4f45e5][default:02840] [ 2] /lib64/libc.so.6(+0x32660)[0x7f516d4f4660][default:02840] [ 3] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZN4Foam8multiplyERNS_5FieldIdEERKN S_5UListIdEES6_+0xd5)[0x7f516e7bfd55][default:02840] [ 4] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so(_ZN4Foam8mult iplyINS_12fvPatchFieldENS_7volMeshEEEvRNS_14Geomet ricFieldIdT_T0_EERKS6_S9_+0x41)[0x7f5172705861][default:02840] [ 5] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so(_ZN4FoammlINS _12fvPatchFieldENS_7volMeshEEENS_3tmpINS_14Geometr icFieldIdT_T0_EEEERKS7_RKS8_+0x15b)[0x7f5172784afb][default:02840] [ 6] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so(_ZN4Foam9RASM odels11RNGkEpsilonINS_29IncompressibleTurbulenceMo delINS_14transportModelEEEE7correctEv+0x2d0)[0x7f51727d5ec0][default:02840] [ 7] buoyantBoussinesqSimpleFoam[0x481a7d][default:02840] [ 8] /lib64/libc.so.6(__libc_start_main+0xfd)[0x7f516d4e0d1d][default:02840] [ 9] buoyantBoussinesqSimpleFoam[0x42db51][default:02840] *** End of error message ***…; Added by Mark JIN at 7:28pm on May 24, 2017

Topic: Butterfly/Openfoam floating issue: ---------------------------------------------------------------*\| ========= | || \\ / F ield | OpenFOAM: The Open Source CFD Toolbox || \\ / O peration | Version: v1612+ || \\ / A nd | Web: www.OpenFOAM.com || \\/ M anipulation | |\*---------------------------------------------------------------------------*/Build : v1612+Exec : buoyantBoussinesqSimpleFoam -parallelDate : May 22 2017Time : 10:18:58Host : "default"PID : 2839Case : /home/ofuser/workingDir/butterfly/simple_hvacnProcs : 4Slaves : 3("default.2840""default.2841""default.2842")Pstream initialized with:floatTransfer : 0nProcsSimpleSum : 0commsType : nonBlockingpolling iterations : 0sigFpe : Enabling floating point exception trapping (FOAM_SIGFPE).fileModificationChecking : Monitoring run-time modified files using timeStampMaster (fileModificationSkew 10)allowSystemOperations : Allowing user-supplied system call operations// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //Create timeCreate mesh for time = 0SIMPLE: convergence criteriafield nut tolerance 0.0001field p_rgh tolerance 0.0001field k tolerance 0.0001field U tolerance 0.0001field T tolerance 0.0001field epsilon tolerance 0.0001field alphat tolerance 0.0001Reading thermophysical propertiesReading field TReading field p_rghReading field UReading/calculating face flux field phiSelecting incompressible transport model NewtonianCreating turbulence modelSelecting turbulence model type RASSelecting RAS turbulence model RNGkEpsilonRNGkEpsilonCoeffs{Cmu 0.0845;C1 1.42;C2 1.68;C3 -0.33;sigmak 0.71942;sigmaEps 0.71942;eta0 4.38;beta 0.012;}Reading field alphatReading gReading hRefCalculating field g.hNo MRF models presentRadiation model not active: radiationProperties not foundSelecting radiationModel noneNo finite volume options presentStarting time loopTime = 1smoothSolver: Solving for Ux, Initial residual = 1, Final residual = 0.06427477, No Iterations 4smoothSolver: Solving for Uy, Initial residual = 1, Final residual = 0.06226344, No Iterations 4smoothSolver: Solving for Uz, Initial residual = 1, Final residual = 0.03950103, No Iterations 3smoothSolver: Solving for T, Initial residual = 1, Final residual = 0.03671111, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 0.008356878, No Iterations 86DICPCG: Solving for p_rgh, Initial residual = 0.07888434, Final residual = 0.0006831407, No Iterations 9DICPCG: Solving for p_rgh, Initial residual = 0.007053905, Final residual = 6.211827e-05, No Iterations 71time step continuity errors : sum local = 3777.266, global = 3.22967, cumulative = 3.22967smoothSolver: Solving for epsilon, Initial residual = 0.9994728, Final residual = 0.0532353, No Iterations 4smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.05640973, No Iterations 4ExecutionTime = 2.65 s ClockTime = 3 sTime = 2smoothSolver: Solving for Ux, Initial residual = 0.5142984, Final residual = 0.02186577, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.5242573, Final residual = 0.02244622, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.5106874, Final residual = 0.02933279, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.3832824, Final residual = 0.01046751, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.9825413, Final residual = 0.009757923, No Iterations 799DICPCG: Solving for p_rgh, Initial residual = 0.04390194, Final residual = 0.000303611, No Iterations 9DICPCG: Solving for p_rgh, Initial residual = 0.0073043, Final residual = 7.259574e-05, No Iterations 45time step continuity errors : sum local = 1883567, global = 2227.205, cumulative = 2230.435smoothSolver: Solving for epsilon, Initial residual = 0.08647006, Final residual = 0.000113174, No Iterations 1smoothSolver: Solving for k, Initial residual = 0.1579946, Final residual = 0.01115579, No Iterations 2ExecutionTime = 9.56 s ClockTime = 10 sTime = 3smoothSolver: Solving for Ux, Initial residual = 0.8070853, Final residual = 0.07865708, No Iterations 3smoothSolver: Solving for Uy, Initial residual = 0.8145663, Final residual = 0.03882168, No Iterations 4smoothSolver: Solving for Uz, Initial residual = 0.5761609, Final residual = 0.0390739, No Iterations 4smoothSolver: Solving for T, Initial residual = 0.1644957, Final residual = 0.006771158, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.7802636, Final residual = 0.006709539, No Iterations 13DICPCG: Solving for p_rgh, Initial residual = 0.04575494, Final residual = 0.0004415382, No Iterations 130DICPCG: Solving for p_rgh, Initial residual = 0.005830491, Final residual = 5.648426e-05, No Iterations 78time step continuity errors : sum local = 6.68889e+12, global = -4.053656e+11, cumulative = -4.053656e+11smoothSolver: Solving for epsilon, Initial residual = 1, Final residual = 0.08337707, No Iterations 1smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.08762031, No Iterations 2ExecutionTime = 11.24 s ClockTime = 11 sTime = 4smoothSolver: Solving for Ux, Initial residual = 0.1870785, Final residual = 0.008250987, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.1039591, Final residual = 0.003633928, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.003344756, Final residual = 0.0001428352, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.0360337, Final residual = 0.0008781286, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.9999995, Final residual = 0.7505781, No Iterations 1001DICPCG: Solving for p_rgh, Initial residual = 2.097918e-11, Final residual = 2.097918e-11, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 2.097918e-11, Final residual = 2.097918e-11, No Iterations 0time step continuity errors : sum local = 9.100777e+16, global = -1.152626e+15, cumulative = -1.153031e+15smoothSolver: Solving for epsilon, Initial residual = 0.006323925, Final residual = 0.0002800085, No Iterations 1smoothSolver: Solving for k, Initial residual = 0.9999998, Final residual = 0.08579136, No Iterations 4ExecutionTime = 15.48 s ClockTime = 16 sTime = 5smoothSolver: Solving for Ux, Initial residual = 0.6268107, Final residual = 0.01889084, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.5691313, Final residual = 0.02593386, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.525286, Final residual = 0.01999095, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.1776883, Final residual = 0.004896742, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.8409992, Final residual = 0.008296552, No Iterations 25DICPCG: Solving for p_rgh, Initial residual = 8.57445e-13, Final residual = 8.57445e-13, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 8.57445e-13, Final residual = 8.57445e-13, No Iterations 0time step continuity errors : sum local = 3.230307e+23, global = -5.044393e+14, cumulative = -1.657471e+15smoothSolver: Solving for epsilon, Initial residual = 4.732135e-05, Final residual = 1.311093e-10, No Iterations 1bounding epsilon, min: -1.103807e+26 max: 1.972571e+51 average: 2.670218e+47smoothSolver: Solving for k, Initial residual = 0.04771126, Final residual = 0.002285774, No Iterations 2ExecutionTime = 16.44 s ClockTime = 17 sTime = 6smoothSolver: Solving for Ux, Initial residual = 0.9995642, Final residual = 0.04432588, No Iterations 4smoothSolver: Solving for Uy, Initial residual = 0.9996968, Final residual = 0.04761556, No Iterations 4smoothSolver: Solving for Uz, Initial residual = 0.9858131, Final residual = 0.06924769, No Iterations 3smoothSolver: Solving for T, Initial residual = 0.01200576, Final residual = 0.0002952721, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.9446084, Final residual = 0.005339222, No Iterations 6DICPCG: Solving for p_rgh, Initial residual = 0.08971123, Final residual = 0.0008218812, No Iterations 6DICPCG: Solving for p_rgh, Initial residual = 0.02323654, Final residual = 0.0002319251, No Iterations 193time step continuity errors : sum local = 4.926861e+44, global = -1.110593e+37, cumulative = -1.110593e+37smoothSolver: Solving for epsilon, Initial residual = 1, Final residual = 0.002671469, No Iterations 2bounding epsilon, min: -2.219668e+47 max: 1.75779e+78 average: 3.182358e+73smoothSolver: Solving for k, Initial residual = 1, Final residual = 0.0501481, No Iterations 2bounding k, min: -3.660183e+25 max: 9.966186e+62 average: 8.53815e+58ExecutionTime = 18.1 s ClockTime = 18 sTime = 7smoothSolver: Solving for Ux, Initial residual = 8.069155e-09, Final residual = 8.069155e-09, No Iterations 0smoothSolver: Solving for Uy, Initial residual = 5.382338e-08, Final residual = 7.473481e-09, No Iterations 1smoothSolver: Solving for Uz, Initial residual = 2.092083e-08, Final residual = 2.077615e-09, No Iterations 1smoothSolver: Solving for T, Initial residual = 0.1619372, Final residual = 0.003564584, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 1, Final residual = 46631.37, No Iterations 1001DICPCG: Solving for p_rgh, Initial residual = 1.64537e-26, Final residual = 1.64537e-26, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 1.64537e-26, Final residual = 1.64537e-26, No Iterations 0time step continuity errors : sum local = 1.468529e+53, global = 5.868436e+40, cumulative = 5.867326e+40smoothSolver: Solving for epsilon, Initial residual = 0.07343377, Final residual = 2.828068e-19, No Iterations 1bounding epsilon, min: -2.257804e+66 max: 8.093947e+109 average: 1.184346e+105smoothSolver: Solving for k, Initial residual = 0.5212037, Final residual = 0.02939162, No Iterations 2ExecutionTime = 22.26 s ClockTime = 22 sTime = 8smoothSolver: Solving for Ux, Initial residual = 0.6924604, Final residual = 0.01784756, No Iterations 2smoothSolver: Solving for Uy, Initial residual = 0.3637153, Final residual = 0.005737122, No Iterations 2smoothSolver: Solving for Uz, Initial residual = 0.2793264, Final residual = 0.00626238, No Iterations 2smoothSolver: Solving for T, Initial residual = 0.07790577, Final residual = 0.002676894, No Iterations 2DICPCG: Solving for p_rgh, Initial residual = 0.8911507, Final residual = 0.008688155, No Iterations 18DICPCG: Solving for p_rgh, Initial residual = 1.957294e-52, Final residual = 1.957294e-52, No Iterations 0DICPCG: Solving for p_rgh, Initial residual = 1.957294e-52, Final residual = 1.957294e-52, No Iterations 0time step continuity errors : sum local = 8.548233e+90, global = -3.056251e+75, cumulative = -3.056251e+75--------------------------------------------------------------------------mpirun noticed that process rank 1 with PID 2840 on node default exited on signal 8 (Floating point exception).--------------------------------------------------------------------------[1] #0 Foam::error:rintStack(Foam::Ostream&)[0] #0 Foam::error:rintStack(Foam::Ostream&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[0] #1 Foam::sigFpe::sigHandler(int) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[1] #1 Foam::sigFpe::sigHandler(int) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[0] #2 ? in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[1] #2 ? in "/lib64/libc.so.6"[0] #3 Foam::multiply(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) in "/lib64/libc.so.6"[1] #3 Foam::multiply(Foam::Field<double>&, Foam::UList<double> const&, Foam::UList<double> const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[0] #4 Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > Foam:perator*<Foam::fvPatchField, Foam::volMesh>(Foam::tmp<Foam::GeometricField<doub le, Foam::fvPatchField, Foam::volMesh> > const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so"[1] #4 void Foam::multiply<Foam::fvPatchField, Foam::volMesh>(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh>&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so"[1] #5 Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > Foam:perator*<Foam::fvPatchField, Foam::volMesh>(Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> const&, Foam::tmp<Foam::GeometricField<double, Foam::fvPatchField, Foam::volMesh> > const&) in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so"[1] #6 Foam::RASModels::RNGkEpsilon<Foam::IncompressibleT urbulenceModel<Foam::transportModel> >::correct() in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so"[1] #7 ? in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/bin/buoyantBoussinesqSimpleFoam"[1] #8 __libc_start_main in "/lib64/libc.so.6"[1] #9 ? in "/opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/bin/buoyantBoussinesqSimpleFoam"[default:02840] *** Process received signal ***[default:02840] Signal: Floating point exception (8)[default:02840] Signal code: (-6)[default:02840] Failing at address: 0x1f400000b18[default:02840] [ 0] /lib64/libc.so.6(+0x32660)[0x7f516d4f4660][default:02840] [ 1] /lib64/libc.so.6(gsignal+0x35)[0x7f516d4f45e5][default:02840] [ 2] /lib64/libc.so.6(+0x32660)[0x7f516d4f4660][default:02840] [ 3] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libOpenFOAM.so(_ZN4Foam8multiplyERNS_5FieldIdEERKN S_5UListIdEES6_+0xd5)[0x7f516e7bfd55][default:02840] [ 4] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so(_ZN4Foam8mult iplyINS_12fvPatchFieldENS_7volMeshEEEvRNS_14Geomet ricFieldIdT_T0_EERKS6_S9_+0x41)[0x7f5172705861][default:02840] [ 5] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so(_ZN4FoammlINS _12fvPatchFieldENS_7volMeshEEENS_3tmpINS_14Geometr icFieldIdT_T0_EEEERKS7_RKS8_+0x15b)[0x7f5172784afb][default:02840] [ 6] /opt/OpenFOAM/OpenFOAM-v1612+/platforms/linux64GccDPInt32Opt/lib/libincompressibleTurbulenceModels.so(_ZN4Foam9RASM odels11RNGkEpsilonINS_29IncompressibleTurbulenceMo delINS_14transportModelEEEE7correctEv+0x2d0)[0x7f51727d5ec0][default:02840] [ 7] buoyantBoussinesqSimpleFoam[0x481a7d][default:02840] [ 8] /lib64/libc.so.6(__libc_start_main+0xfd)[0x7f516d4e0d1d][default:02840] [ 9] buoyantBoussinesqSimpleFoam[0x42db51][default:02840] *** End of error message ***…; Added by Mark JIN to Ladybug Tools at 1:51am on May 31, 2017

Comment on: Topic 'Baking Breps w/ Color - RHINOCOMMON': es only have one raison d'être, which is to group types into logical chunks. A Type is the definition of a class or a structure. Classes and structures are very similar entities (they can both contain any number of methods, properties and other types), but because they behave differently, you need to know which is which. An Instance of a type is a single object that actually exists. For example, the class Human is the definition of what it means to be human. You are an instance of this class. I am a different instance of this class. Damien is yet another instance of this class. Every instance can assign unique values to all its properties and fields. If for example the type Human had a property for height, then in my case it would say 1.97m. In Damien's case it would be set to something much less, as Damien isn't anywhere near as handsome and tall as I am. A Reference is a piece of information that tells you where a certain instance is. Think of a reference as an address. When you mail a letter (or e-mail), you must specify a valid and unambiguous address or the letter won't arrive. Similarly, every piece of data stored in the memory of your computer also has a unique address, but instead of "3670, Woodland Park Avenue, Seattle", it looks like this 0x12345678. Trying to access an instance through an invalid reference is like sending a letter without an address. References are sometimes also called "variables", though sometimes the word variable is only used to indicate primitive types, such as Booleans, Integers and such. A reference is not the instance itself. Take the following code: 1. Dim crv As Rhino.Geometry.Curve 2. Dim dup As Rhino.Geometry.Curve 3. crv = GetACurveFromSomewhere() 4. dup = crv 5. If (dup IsNot Nothing) Then dup = dup.DuplicateCurve() One lines (1) and (2) I declare two references, one is called "crv", the other "dup". Because Visual Basic is a strongly typed language, I can assign limitations to what sort of data crv and dup are allowed to reference. In this case they can only point to instances of the Rhino.Geometry.Curve class or any class which derives from Rhino.Geometry.Curve (such as Rhino.Geometry.NurbsCurve, or Rhino.Geometry.LineCurve). On line (3) I assign an actual curve instance to the crv reference/variable. At least, assuming the GetACurveFromSomewhere() function actually returns a proper instance. If it doesn't, crv will remain a "null reference". Line (4) is interesting, because both crv and dup will now point to the same curve instance. So even though there is only 1 curve in memory, both crv and dup provide access to it. This means that when we change the curve via crv, then dup will notice that change. On line (5) two things happen. I want to duplicate my curve data so I can change the data via dup, without affecting the data available via crv. The best way to duplicate a curve (i.e. create a second curve in memory, that has the same shape as the first curve) is to use the DuplicateCurve() method on the Rhino.Geometry.Curve class. However I cannot call a method on an instance that doesn't exist, so before I do that, I need to check whether or not dup actually points to a real curve object, or whether it is a null reference. Finally, it is also possible to have an instance of a class in memory, without any references to it. In this case nobody can reach that curve any more and it is essentially dead weight, taking up pointless memory. In C++ this is called a Memory Leak and it's considered a serious bug. In VB.NET and C# this memory will automatically be cleaned up by the .NET Garbage Collector. In my opinion the Garbage Collector is the single most important feature in .NET. It's what turns VB and C# from frustration central into a friendly and flexible coding platform. -- David Rutten david@mcneel.com Poprad, Slovakia…; Added by David Rutten at 4:10pm on August 9, 2011