EP output variables are to calculate outdoorAirEnergy?
Thank you very much!
Output variables on the Read EP Results component:[1] totalThermalEnergy=cooling+heating[2] thermalEnergyBalance=cooling (-)andheating (+)[3] cooling= Zone Ideal Loads Supply Air Total Cooling Energy [J](Hourly)=Zone Ideal Loads Supply Air Sensible Cooling Energy [J](Hourly)+ Zone Ideal Loads Supply Air Latent Cooling Energy [J](Hourly)[4] heating= Zone Ideal Loads Supply Air Total Heating Energy [J](Hourly)= Zone Ideal Loads Supply Air Sensible Heating Energy [J](Hourly) + Zone Ideal Loads Supply Air Latent Heating Energy [J](Hourly)[5] electricLight=Zone Lights Electric Energy [J](Hourly)[6] electricEquip=Electric Equipment Electric Energy [J](Hourly)[7] peopleGains=Zone People Total Heating Energy [J](Hourly)[8] totalSolarGain=Zone Windows Total Transmitted Solar Radiation Energy[9] infiltrationEnergy=Zone Infiltration Total Heat Gain Energy (+)andZone Infiltration Total Heat Loss Energy (-)[10] outdoorAirEnergy= ???[11] natVentEnergy=Zone Ventilation Total Heat Gain Energy (+)andZone Ventilation Total Heat Loss Energy (-)[12] operativeTemperature=Zone Operative Temperature[13] airTemperature=Zone Mean Air Temperature[14] meanRadTemperature=Zone Mean Radiant Temperature[15] relativeHumidity=Zone Air Relative Humidity[16] airFlowVolume=[infiltrationFlow] Zone Infiltration Standard Density Volume Flow Rate+[natVentFlow] Zone Ventilation Standard Density Volume Flow Rate+[mechSysAirFlow] Zone Mechanical Ventilation Standard Density Volume Flow Rate+[earthTubeFlow] Earth Tube Air Flow Volume[17] airHeatGainRate=[surfaceAirGain] Zone Air Heat Balance Surface Convection Rate+[systemAirGain] Zone Air Heat Balance System Air Transfer Rate
Output variables on the Read EP Surface Results component:[1] surfaceIndoorTemp= Surface Inside Face Temperature[2] surfaceOutdoorTemp=Surface Outside Face Temperature[3] surfaceEnergyFlow=[opaqueEnergyFlow] Surface Average Face Conduction Heat Transfer Energy+[glazEnergyFlow] Surface Window Heat Gain Energy[4] opaqueEnergyFlow =Surface Average Face Conduction Heat Transfer Energy[5] glazEnergyFlow= Surface Window Heat Gain Energy[6] windowTotalSolarEnergy=Surface Window Transmitted Solar Radiation Energy[7] windowBeamEnergy=Surface Window Transmitted Beam Solar Radiation Energy[8] windowDiffEnergy=Surface Window Transmitted Diffuse Solar Radiation Energy[9] windowTransmissivity=Surface Window System Solar Transmittance…
was not all there myself. Overall the night wasn't that productive so I wanted to apologize, I will do a better job in the future.
Attached to this message is the Assignment sheet for the upcoming week. Please post the picture of the models before 7:00 PM Monday 2/16.
Here is a link to the completed script from last night, as well as the Rhino file and presentation pdf.
https://www.dropbox.com/sh/3g6fnue93dk8iub/AAB88CNVCtC64cmz_ENLlojQa?dl=0
A few notes:
- I added two separate tags to the end of the script. One set is for the 3D model of your form, locating where the pieces originally come from. The second set is for the flattened out sections, which can be etched on your pieces to actually locate them when they are physically created. Play around a bit in the script and try to understand what is going on between the different parts.
-Baking: We went over baking in last weeks class. You right click on the component you want in the physical realm and select bake. Rhino will then ask you to select a layer to place the items on. I would suggest having two layers, one will be for cutting and one will be for etching (when you bake the tags(optional)). Once the pieces are in Rhino, you can use the Make2d command and export to AutoCad where you can laser cut (if you are unsure about this process, Google it as there are numerous tutorials).
-I would recommend using chipboard as it is the cheapest and most readily available, but don't let me chain your creativity if you come up with another material.
I look forward to seeing your guys models. See you Monday!
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mainly grasshopper. (If it were just Rhino it perhaps would have been easier for me). I've been working on it for a while now and I unfortunately am a bit stuck.
Below are some of my concerns:
1) I know the theory of what I'm suppose to do which is to have the rectangular base and scale it then array it up. However I noticed that the thickness of the each lath and support varies. There are 25 laths in all and from the structure diagram I have gathered that there are basically 4 groups of the same thickness from the base going up its the first 9, then 7, then 5 and then the top 3. I just can't seem to figure out how to vary the thickness. I would assume the attached lath and support definition diagrams would help but unfortunately I don't know how to read it. I've tried some formulas which didn't exactly work but I still included them in the file.
2) I also need to figure out how to create the hole in the structure which is the entrance. I know in Rhino I could just Boolean it out but is there a way to do it in grasshopper?
3) I also need helping figuring out the definition for putting the vertical supports in between each row. The diagram says something fancy about "Testing acceptable constraints in flexion and in shear, we find an acceptable eccentricity that varies with each row." Ok maybe it wasn't so fancy but I have no clue how to do that with grasshopper!
4) My lecturer wants a Structure Simulation which I'm going to assume is what number 3 is all about?
I've attached my progress so far and would appreciate any help possible. I'd prefer if anyone could guide me using basic things (without any fancy plug-ins unless it's absolutely necessary).
However, any help is appreciated! Thank you so much in advance.
Cheers!
Jo
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st variety of papers (mostly related with LIDAR airborne sampled clouds) ... but ... hmm ... no code (other than some "abstract" algos that may (or may not) work). Reason? A very hot cake that one these days: from reverse engineering to DARPA founded future defense systems and up to cruse missiles pattern recognition algos.
The solution (obviously doable only via code) is the so called flat hard clustering ... were points are sampled into clusters based on the coPlanarity "rule". For large amounts recursive octTrees (an oriented box divided in 8 "partitions") subdivisions are used and then pts are processed in parallel (and then clusters are re-evaluated in order to "absorb" other clusters with same plane A,B,C,D vars etc etc).
See what's happening in a very carefully made test point collection:
3.7 ms and the "ideal" clustering (7 search loops VS the max 42M theoretical threshold):
Depending on the pts "preparation" ... a considerable more time/search loops is required ... and ... well ... also "valid" clusters (4 points and up) made:
So "ideally" speaking in your case:
1. Mesh faces center points (or alternatively: mesh vertices) are sampled into a pts collection .
2. Hard flat coPlanarity clustering is attempted yielding pts/planes in equivalent DataTrees.
3. Planar Breps are made with respect the planes (like the black things captured above) and sampled, say, into a breps List.
4. The method Brep[] solids = Brep.CreateSolid(breps); is used for attempting to create your desired "engulfing" brep. This method is very slow mind (other waaaay faster approaches also available).
…
decided to concentrate my effort today on this problem and manage to come up with a solution !
I will explain it if somebody else is looking for a similar solution.
Finally my only problem was to create an alternating true/false list that inverse at certain index, this what I came up with: I have a list of points and random index , the box and sphere represent true and false, and the blue sphere is the node(index) where I want to see an inversion.
In reality, it was pretty simple, I just didn't know the right modules. (In yellow, it's the most important part of the patch)(Sorry for the spelling mistake)
Here is a diagram of what I did: I created a list going to 1 to [number of lines], here it's 1 to 10, I had node at 3-4 and 7-8. For each node I created a list of 1 repeated [(number of lines)-index] times. Here, 7 (10-3) and 3 (10-7) times.
After grafting everything, I add everything in mass addition module. I had my final list which I checked if it was divisible by two.
It was more of a logic problem than a grasshopper problem.
Here it is the initial shape with what I wanted !
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The PC actually stops working because after a few seconds the simulation starts the fan inside the PC all of a sudden stops and for the next 5-10 mins I cannot do anything, even alt+ctrl+canc. After I wait for that time i get the followig error:
the ReadMe says:
{0;0;0}0. Grid-based Radiance simulation1. The component is checking ad, as, ar and aa values. This is just to make sure that the results are accurate enough.2. -ar is set to 300.3. Good to go!4. Current working directory is set to: C:\Users\Luigi\Desktop\Prova__\Prova_1\gridBasedSimulation\5. Found a trans material... Resetting st parameter from 0.85 to 0.011276004966. WMIC PROCESS get Commandline7. WMIC PROCESS get Commandline8. WMIC PROCESS get Commandline9. WMIC PROCESS get Commandline10. WMIC PROCESS get Commandline11. WMIC PROCESS get Commandline12. WMIC PROCESS get Commandline13. WMIC PROCESS get Commandline14. WMIC PROCESS get Commandline15. WMIC PROCESS get Commandline16. WMIC PROCESS get Commandline17. WMIC PROCESS get Commandline18. WMIC PROCESS get Commandline19. WMIC PROCESS get Commandline20. WMIC PROCESS get Commandline21. WMIC PROCESS get Commandline22. WMIC PROCESS get Commandline23. WMIC PROCESS get Commandline24. WMIC PROCESS get Commandline25. WMIC PROCESS get Commandline26. WMIC PROCESS get Commandline27. WMIC PROCESS get Commandline28. WMIC PROCESS get Commandline29. WMIC PROCESS get Commandline30. WMIC PROCESS get Commandline31. WMIC PROCESS get Commandline32. WMIC PROCESS get Commandline33. WMIC PROCESS get Commandline34. WMIC PROCESS get Commandline35. WMIC PROCESS get Commandline36. WMIC PROCESS get Commandline37. WMIC PROCESS get Commandline38. WMIC PROCESS get Commandline39. WMIC PROCESS get Commandline40. WMIC PROCESS get Commandline41. WMIC PROCESS get Commandline42. WMIC PROCESS get Commandline43. WMIC PROCESS get Commandline44. WMIC PROCESS get Commandline45. WMIC PROCESS get Commandline46. WMIC PROCESS get Commandline47. WMIC PROCESS get Commandline48. WMIC PROCESS get Commandline49. WMIC PROCESS get Commandline50. WMIC PROCESS get Commandline51. WMIC PROCESS get Commandline52. WMIC PROCESS get Commandline53. WMIC PROCESS get Commandline54. WMIC PROCESS get Commandline55. WMIC PROCESS get Commandline56. WMIC PROCESS get Commandline57. WMIC PROCESS get Commandline58. WMIC PROCESS get Commandline59. WMIC PROCESS get Commandline60. WMIC PROCESS get Commandline61. WMIC PROCESS get Commandline62. WMIC PROCESS get Commandline63. WMIC PROCESS get Commandline64. WMIC PROCESS get Commandline65. WMIC PROCESS get Commandline66. WMIC PROCESS get Commandline67. WMIC PROCESS get Commandline68. WMIC PROCESS get Commandline69. WMIC PROCESS get Commandline70. WMIC PROCESS get Commandline71. WMIC PROCESS get Commandline72. WMIC PROCESS get Commandline73. WMIC PROCESS get Commandline74. WMIC PROCESS get Commandline75. WMIC PROCESS get Commandline76. WMIC PROCESS get Commandline77. WMIC PROCESS get Commandline78. WMIC PROCESS get Commandline79. WMIC PROCESS get Commandline80. WMIC PROCESS get Commandline81. WMIC PROCESS get Commandline82. WMIC PROCESS get Commandline83. WMIC PROCESS get Commandline84. WMIC PROCESS get Commandline85. WMIC PROCESS get Commandline86. WMIC PROCESS get Commandline87. WMIC PROCESS get Commandline88. WMIC PROCESS get Commandline89. WMIC PROCESS get Commandline90. WMIC PROCESS get Commandline91. WMIC PROCESS get Commandline92. WMIC PROCESS get Commandline93. WMIC PROCESS get Commandline94. WMIC PROCESS get Commandline95. WMIC PROCESS get Commandline96. WMIC PROCESS get Commandline97. WMIC PROCESS get Commandline98. WMIC PROCESS get Commandline99. WMIC PROCESS get Commandline100. WMIC PROCESS get Commandline101. WMIC PROCESS get Commandline102. WMIC PROCESS get Commandline103. WMIC PROCESS get Commandline104. WMIC PROCESS get Commandline105. WMIC PROCESS get Commandline106. WMIC PROCESS get Commandline107. WMIC PROCESS get Commandline108. WMIC PROCESS get Commandline109. WMIC PROCESS get Commandline110. WMIC PROCESS get Commandline111. WMIC PROCESS get Commandline112. WMIC PROCESS get Commandline113. WMIC PROCESS get Commandline114. WMIC PROCESS get Commandline115. WMIC PROCESS get Commandline116. WMIC PROCESS get Commandline117. WMIC PROCESS get Commandline118. WMIC PROCESS get Commandline119. WMIC PROCESS get Commandline120. WMIC PROCESS get Commandline121. WMIC PROCESS get Commandline122. WMIC PROCESS get Commandline123. WMIC PROCESS get Commandline124. WMIC PROCESS get Commandline125. WMIC PROCESS get Commandline126. WMIC PROCESS get Commandline127. WMIC PROCESS get Commandline128. WMIC PROCESS get Commandline129. WMIC PROCESS get Commandline130. WMIC PROCESS get Commandline131. WMIC PROCESS get Commandline132. WMIC PROCESS get Commandline133. WMIC PROCESS get Commandline134. WMIC PROCESS get Commandline135. WMIC PROCESS get Commandline136. WMIC PROCESS get Commandline137. WMIC PROCESS get Commandline138. WMIC PROCESS get Commandline139. WMIC PROCESS get Commandline140. WMIC PROCESS get Commandline141. WMIC PROCESS get Commandline142. WMIC PROCESS get Commandline143. WMIC PROCESS get Commandline144. WMIC PROCESS get Commandline145. WMIC PROCESS get Commandline146. WMIC PROCESS get Commandline147. WMIC PROCESS get Commandline148. WMIC PROCESS get Commandline149. WMIC PROCESS get Commandline150. WMIC PROCESS get Commandline151. WMIC PROCESS get Commandline152. WMIC PROCESS get Commandline153. WMIC PROCESS get Commandline154. WMIC PROCESS get Commandline155. WMIC PROCESS get Commandline156. WMIC PROCESS get Commandline157. WMIC PROCESS get Commandline158. WMIC PROCESS get Commandline159. WMIC PROCESS get Commandline160. WMIC PROCESS get Commandline161. WMIC PROCESS get Commandline162. WMIC PROCESS get Commandline163. WMIC PROCESS get Commandline164. WMIC PROCESS get Commandline165. WMIC PROCESS get Commandline166. WMIC PROCESS get Commandline167. WMIC PROCESS get Commandline168. WMIC PROCESS get Commandline169. WMIC PROCESS get Commandline170. WMIC PROCESS get Commandline171. WMIC PROCESS get Commandline172. WMIC PROCESS get Commandline173. WMIC PROCESS get Commandline174. WMIC PROCESS get Commandline175. WMIC PROCESS get Commandline176. WMIC PROCESS get Commandline177. WMIC PROCESS get Commandline178. WMIC PROCESS get Commandline179. WMIC PROCESS get Commandline180. WMIC PROCESS get Commandline181. WMIC PROCESS get Commandline182. WMIC PROCESS get Commandline183. WMIC PROCESS get Commandline184. WMIC PROCESS get Commandline185. WMIC PROCESS get Commandline186. WMIC PROCESS get Commandline187. WMIC PROCESS get Commandline188. WMIC PROCESS get Commandline189. WMIC PROCESS get Commandline190. WMIC PROCESS get Commandline191. WMIC PROCESS get Commandline192. WMIC PROCESS get Commandline193. WMIC PROCESS get Commandline194. WMIC PROCESS get Commandline195. WMIC PROCESS get Commandline196. WMIC PROCESS get Commandline197. WMIC PROCESS get Commandline198. Runtime error (IndexOutOfRangeException): index out of range: 0199. Traceback: line 320, in script
The thing is that if I raise the -aa parameter from 0.05 to 0.1 all works fine..
Is this only related to my PC then?? What should I do to solve this issue?
Thanks again for your help
Luigi…
rves that "intersect" a plane placed on Z=6 above the first circle. I did this to have a collection of points from which to choose 3 and make a 3pt-circle.
[this second circle "fits" the catenary at a certain height, that's what I wanted to do]
Maybe it's obtuse but anyway that's the way I managed it.. I then used the "intersection" of the top circle with the original catenary curve to "split" the catenary into 2 parts, I then "Rail Revolution" the first part of it around the axis of the original circle, using the circle as a "rail", and I get a Brep surface.
It is a "open brep" surface, so now i'm having the problem of managing it if I want to subdivide it with Isotrim or other commands to control the number of subdivisions.
Is there a better way to go about this?
I am attaching the file.
About the image, I checked my code about 10 times to understand why it has those "lines" every 1 meter in the Z, and they already appear in the "rail revolution" component when it is visible, but in the "brep components" I can see the individual points along the rail curve.
I think this is what might be causing the brep to surface problem, but for the life of me I can't understand why the rail is not smooth and is "divided" into the 7 points instead of just one smooth revolution...
Thanks! :)
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rder to deal with the contents of the MERO structure (like glass, panels, polycarbonate). That is what the C# does already.
3. Vectors (a la "Umbrella" sticks) in order to place correctly your MERO nodes (the "hexagon" brackets - so to speak). That is what the big C# (the one that I've send to you some time ago) does already.
4. Calculations (lengths, angles) for each node against the other related nodes and the points derived from dividing the MERO square "tubes". For a given node these points are variable (from 2 [when in the "bounds" of mesh] to 6 ["typical" middle point, so to speak].
5. Demo block instances in order to see first hand what GH can actually do (that's WOW stuff: you slide a slider and "several" real-life components are placed in 3d space in real-time, he he).
6. Node connectivity data for the obvious (assembling the MERO on site).
7. Some assembly "simulation" capability (we do this today and this tomorrow ...)
So forget the single carrot (plenty carrots for you soon) for a while and answer to the most critical question: Based on what you've displayed to me (Skype) what is your policy against the MERO node itself?
I mean: we don't deal with a classic MERO ball type here (meaning variable drilling axis per ball). Meaning that the "hexagon" bracket (if I may use the term) IS VARIABLE. Meaning: you need a "module" that can being adapted against "every" possible (logical) angle value? (and compose the bracket?) Or you gonna fabricate the "brackets" on a per node basis?
And what if we had a planar glazing system? (same principle, more expensive, 100 times more WOW).
BTW: The best man in the world to do "similar things" with "hinged" custom aluminum systems (like doing the blue facade that you've displayed to me with some semi structural/structural system) he's a very close friend of mine. He's based in Dubai UAE.…
ate):
1) go to: https://github.com/mostaphaRoudsari/ladybug/2) click on "clone or download"/Download ZIP
3) Download and extract the folder wherever you want on your machine
4) Open the folder and open "userObjects"
5) you'll see something like this
6) open Grasshopper/File/Special Folders/User Object Folder
7) Select and delete all Ladybug components
8) Drag all components of the point 5) into the canvas of Grasshopper wherever you want or inside the "User Object Folder"... it is the same thing.
And it should be fine.
Let me know if it works.
Best
Antonello
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requiredKeys_ input of the "OSM Shapes" component. This is not the source of your problem though, but still I mentioned it in case you solve your issue, and afterwards want to use the "OSM Shapes" component.
The current (Win32Exception): WindowsError is the very same error message that you reported back in February.For some reason, your Windows is not allowing the Gismo "OSM Shapes" component to delete C:\MapWinGIS_installation_folder\gdal-data\osmconf.ini file.
You previously solved it by allowing the full access control to it, so I am not sure why it is not working now.Windows 10 seems to be the most overprotected operating system among other Windows versions, at least judging by the questions people asked so far.
Maybe you can try to turn off all the services which prevent users from changing certain files, like UAC or maybe even your antivirus?
Try this:
1) Close your Grasshopper and Rhino.2) Restart your PC3) When it boots up again, in your Start menu's search box type: "UAC". Click on it, and a new User Account Control Settings window will open. Set the bar on the left to "Never notify".4) Completely turn off your Antivirus.5) Check once again if your access control to the C:\MapWinGIS_installation_folder\gdal-data\osmconf.ini file is still set to the values you previously reported in this post.6) Right-click on "Rhino 5" icon and then choose: "Run as administrator".7) When Rhino boots up, run Grasshopper, and open the newest create_3dbuildings_trees_streets.gh file from here.If none of this helps, maybe you have some other application which deals with access to files on your system? Malware removal application or similar? Try turning it off too.…
Added by djordje to Gismo at 9:10am on April 3, 2017