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March 9, 2009, 11:30 |
I everybody.
Just a quick q
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#101 |
Member
antonio segalini
Join Date: Mar 2009
Posts: 75
Rep Power: 17 |
I everybody.
Just a quick question: if I have a 2d geometry with a single cell with thickness 2.5mm in the Z direction and I run the forces utility, the torque will be the one generated by those 2.5 mm. So, if I want the torque generated for 1 meter depth, I have to multiply for 400. Is that correct? |
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March 9, 2009, 19:41 |
hei, Antonio,
My experiment w
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#102 |
Member
Hai Yu
Join Date: Mar 2009
Location: Harbin
Posts: 67
Rep Power: 17 |
hei, Antonio,
My experiment with depth 0.1M leads to a 1/10 torque comparing with Fluent. I think most times, it is right. |
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March 19, 2009, 00:42 |
error in lift drag compilation
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#103 |
New Member
leo paul
Join Date: Mar 2009
Posts: 6
Rep Power: 17 |
hi,
I was following Srinath's procedure for compilation of liftdrag tool in of1.4.everything went ok till step 6 where after executing ./Allwmake i find that all other files except liftdrag.o are created and i get the following error message..its quite long! but since i've very little knowledge in o.f or ubuntu for that matter i decided to put the whole thing in..please help me out!! P.S:the entire error message was too long ..i've taken bits from the start and the end..i hope this is a relevant post cause it deals with forces!ive searched the forum and no ones got this error |
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March 20, 2009, 09:41 |
error in liftdrag compilation
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#104 |
New Member
leo paul
Join Date: Mar 2009
Posts: 6
Rep Power: 17 |
hi,
this is the entire error message. thanks. leo |
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March 20, 2009, 13:29 |
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#105 |
Senior Member
Niels Gjoel Jacobsen
Join Date: Mar 2009
Location: Copenhagen, Denmark
Posts: 1,902
Rep Power: 37 |
Hi Leo
You are missing your headers files. Install using: sudo apt-get install build-essential and you should be able to compile. Best regards, Niels |
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March 20, 2009, 16:00 |
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#106 |
Senior Member
Srinath Madhavan (a.k.a pUl|)
Join Date: Mar 2009
Location: Edmonton, AB, Canada
Posts: 703
Rep Power: 21 |
I think you have your answer now :-)
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March 21, 2009, 12:53 |
Thank you
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#107 |
New Member
leo paul
Join Date: Mar 2009
Posts: 6
Rep Power: 17 |
hi,
Thanks a lot guys...will try that out.. Leo |
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March 21, 2009, 14:51 |
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#108 |
New Member
leo paul
Join Date: Mar 2009
Posts: 6
Rep Power: 17 |
hi,
compiled succesfully..had to copy that foamutil file frm of1.2 as said in 1 of the posts after step7 tho..nw i've t fix the bug i guess and start off..thanks again guys.. Leo. |
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March 27, 2009, 04:43 |
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#109 |
Member
Marco Müller
Join Date: Mar 2009
Location: Germany
Posts: 94
Rep Power: 17 |
Richard Samuel: Why is the the forceCoeff for an axisymmetric case calculated wrong? For example a infinite long circular cylinder in 2D as a half model?!
And how is your patch executed?? Thanks, Marco |
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April 8, 2009, 15:17 |
interFoam forces
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#110 |
Senior Member
Tomislav Maric
Join Date: Mar 2009
Location: Darmstadt, Germany
Posts: 284
Blog Entries: 5
Rep Power: 21 |
Hello everyone,
I'm trying to do a simulation of a ship on a free surface using interFoam and calculate the forces. I'm running 32bit Ubuntu 8.10 on Hp Compaq 6820s laptop with latest OpenFOAM-1.5-dev from the repo. This is what I've added to my controlDict: functions ( forces { type forces; functionObjectLibs ("libforces.so"); patches (Hull_OBJECT); rhoInf 1000; CofR (0 0 0); } ); and this is the error I get: (snipped the header) Create time Create mesh for time = 0 Reading environmentalProperties Reading field pd Reading field gamma Reading field U Reading/calculating face flux field phi Reading transportProperties Selecting incompressible transport model Newtonian Selecting incompressible transport model Newtonian Calculating field g.h time step continuity errors : sum local = 3.71483e-07, global = 4.68522e-11, cumulative = 4.68522e-11 PCG: Solving for pcorr, Initial residual = 1, Final residual = 8.66164e-11, No Iterations 204 time step continuity errors : sum local = 3.21776e-17, global = 2.07916e-19, cumulative = 4.68522e-11 Courant Number mean: 0.0005283 max: 0.00883279 velocity magnitude: 7.49691 Starting time loop Courant Number mean: 0.010566 max: 0.176656 velocity magnitude: 7.49691 deltaT = 0.02 Time = 0.02 MULES: Solving for gamma Liquid phase volume fraction = 0.790868 Min(gamma) = -6.562e-19 Max(gamma) = 1 MULES: Solving for gamma Liquid phase volume fraction = 0.790866 Min(gamma) = -1.18035e-18 Max(gamma) = 1 PCG: Solving for pd, Initial residual = 0.999223, Final residual = 0.023873, No Iterations 3 PCG: Solving for pd, Initial residual = 0.0133212, Final residual = 0.000661896, No Iterations 13 PCG: Solving for pd, Initial residual = 0.00127542, Final residual = 9.36798e-08, No Iterations 150 time step continuity errors : sum local = 1.18414e-07, global = 4.01111e-10, cumulative = 4.47963e-10 ExecutionTime = 40.54 s ClockTime = 46 s Courant Number mean: 0.0118945 max: 0.811429 velocity magnitude: 57.9195 deltaT = 0.01 keyword nu is undefined in dictionary "/home/tomislav/OpenFOAM/tomislav-1.5-dev/run/semestralniProjekt/brod_interFoam/constant/transportProperties" file: /home/tomislav/OpenFOAM/tomislav-1.5-dev/run/semestralniProjekt/brod_interFoam/constant/transportProperties from line 21 to line 32. From function dictionary::lookupEntry(const word& keyword) const in file db/dictionary/dictionary.C at line 213. FOAM exiting tomislav@icarus:brod_interFoam$ *** glibc detected *** /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/applications/bin/linuxGccDPOpt/interFoam: double free or corruption (fasttop): 0x0adb26b0 *** ======= Backtrace: ========= /lib/tls/i686/cmov/libc.so.6[0xb6be6454] /lib/tls/i686/cmov/libc.so.6(cfree+0x96)[0xb6be84b6] /home/tomislav/Software/gcc-4.3.3/lib/libstdc++.so.6(_ZdlPv+0x21)[0xb6dd4271] /home/tomislav/Software/gcc-4.3.3/lib/libstdc++.so.6(_ZNSs4_Rep10_M_destroyERKSaIcE+0x1d )[0xb6db27cd] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libinterfaceProperties.so(_ZN4Foam4wordD1Ev+0x63)[0xb7ed26f3] /lib/tls/i686/cmov/libc.so.6(exit+0x89)[0xb6ba5d89] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libOpenFOAM.so(_ZN4Foam7IOerror4exitEi+0x20a)[0xb6f437ba] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libOpenFOAM.so(_ZNK4Foam10dictionary11lookupEntryE RKNS_4wordEb+0xec)[0xb6f8df7c] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libOpenFOAM.so(_ZNK4Foam10dictionary6lookupERKNS_4 wordEb+0x2c)[0xb6f8dfbc] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libforces.so(_ZNK4Foam6forces10devRhoReffEv+0xee5)[0xb0bee085] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libforces.so(_ZNK4Foam6forces16calcForcesMomentEv+ 0xc8)[0xb0bee528] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libforces.so(_ZN4Foam6forces5writeEv+0x52)[0xb0bec112] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libforces.so(_ZN4Foam26OutputFilterFunctionObjectI NS_6forcesEE7executeEv+0x56)[0xb0c0e176] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libOpenFOAM.so(_ZN4Foam18functionObjectList7execut eEv+0x6b)[0xb6fb136b] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libOpenFOAM.so(_ZN4Foam4TimeppEv+0x48)[0xb6fb93d8] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libOpenFOAM.so(_ZN4Foam4TimeppEi+0x11)[0xb6fb9131] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/applications/bin/linuxGccDPOpt/interFoam[0x80641bb] /lib/tls/i686/cmov/libc.so.6(__libc_start_main+0xe5)[0xb6b8d685] /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/applications/bin/linuxGccDPOpt/interFoam[0x8061551] ======= Memory map: ======== 08048000-080da000 r-xp 00000000 08:03 7358876 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/applications/bin/linuxGccDPOpt/interFoam 080da000-080dc000 rw-p 00091000 08:03 7358876 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/applications/bin/linuxGccDPOpt/interFoam 09c63000-0b537000 rw-p 09c63000 00:00 0 [heap] aba96000-abec3000 rw-p aba96000 00:00 0 ac6f5000-acf27000 rw-p ac6f5000 00:00 0 ad352000-ad77f000 rw-p ad352000 00:00 0 adbac000-aedb5000 rw-p adbac000 00:00 0 af8e3000-afce8000 rw-p af8e3000 00:00 0 b0115000-b026c000 rw-p b0115000 00:00 0 b03c3000-b07f0000 rw-p b03c3000 00:00 0 b0b3a000-b0bd9000 r-xp 00000000 08:03 18745 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libLESfilters.so b0bd9000-b0bdb000 rw-p 0009e000 08:03 18745 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libLESfilters.so b0bdb000-b0c1b000 r-xp 00000000 08:03 18755 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libforces.so b0c1b000-b0c1c000 rw-p 00040000 08:03 18755 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libforces.so b0c1c000-b0c1d000 rw-p b0c1c000 00:00 0 b0ecb000-b144f000 rw-p b0ecb000 00:00 0 b18cc000-b19cd000 r-xp 00000000 08:03 18748 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libcompressibleLESModels.so b19cd000-b19d1000 rw-p 00100000 08:03 18748 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libcompressibleLESModels.so b19d1000-b1b4f000 r-xp 00000000 08:03 18744 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libcompressibleRASModels.so b1b4f000-b1b52000 rw-p 0017e000 08:03 18744 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libcompressibleRASModels.so b1b52000-b1ca9000 rw-p b1b52000 00:00 0 b1e30000-b1e56000 r-xp 00000000 08:03 18746 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libLESdeltas.so b1e56000-b1e57000 rw-p 00026000 08:03 18746 /home/tomislav/OpenFOAM/OpenFOAM-1.5-dev/lib/linuxGccDPOpt/libLESdeltas.so b1e57000-b1e97000 r-xp 00000000 08:03 18728 /home/tomislav ... and so on.... I've tried using forces in icoFoam as a test and everything worked ok, as with simpleFoam. I even have a Python script somewhere that extracts the data for nice plots of calculated magnitudes of both forces and moments. Email me and I'll send what I have. The forces directory is written, but since the simulation stops before first timeStep it contains only the title comment of the forces and moments components. From what little I understand C++ i think that the code is having trouble seeing through nested dict-s in transport properties. But if so, why doesn't it complain in the start at "reading transportProperties"? Should I tamper with the source code to adjust it for interFoam? Has anyone seen this before? What's with the glibc error? I've had the same error using other solvers, but they ended normaly, and the forces directory was written. I've tried to build it using wmake, and it was up to date (as expected, since it works fine with other solvers). I've deleted the functions entry in controlDict and the simulation is running fine for a whole day. Tomislav |
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April 8, 2009, 16:49 |
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#111 |
Senior Member
Tomislav Maric
Join Date: Mar 2009
Location: Darmstadt, Germany
Posts: 284
Blog Entries: 5
Rep Power: 21 |
to answer myself: forces lib has trouble finding the right nu in the transportProperties dict for interFoam cases.
in the ~/OpenFOAM/OpenFOAM-1.5-dev/src/postProcessing/forces/forces.C go to line number 101 and look around else if (obr_.foundObject<dictionary>("transportProperties ")) { const dictionary& transportProperties = obr_.lookupObject<dictionary>("transportProperties "); // This is really stupid: it presumes that the water is the // phase1 (just like damBreak tutorial), and takes it's // viscosity for reference calculation. dimensionedScalar nu(transportProperties.lookupEntry("phase1").dict( ).lookup("nu")); // ORIGINAL line is this one below //dimensionedScalar nu(transportProperties.lookup("nu")); const volVectorField& U = obr_.lookupObject<volVectorField>(Uname_); return -rhoRef_*nu*dev(twoSymm(fvc::grad(U))); } I've commented the original troublesome part: //ORIGINAL line //dimensionedScalar nu(transportProperties.lookup("nu")); because it tries to search for "nu" in transportProperties, and "nu" is nested within "phase1" or "phase2" subdictionary, so I've added this: dimensionedScalar nu(transportProperties.lookupEntry("phase1").dict( ).lookup("nu")); and it works now (writes the forces in forces directory). The downside to this stupid solution is that you write forces for the phase1. In my case it's the forces imposed by the water, because these forces are kind of important for a ship (at least i think so ). Does anyone have any suggestion or comment on this? I think this solves my problem for now, but I'm not even sure of that. Awaiting for floating point exception error, Tomislav |
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May 6, 2009, 09:46 |
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#112 |
Senior Member
Daniel WEI (老魏)
Join Date: Mar 2009
Location: Beijing, China
Posts: 689
Blog Entries: 9
Rep Power: 21 |
oops, I'm late again to join the discussion.
libforces.so works fine for me, I think it's better than the old liftDrag utility, very flexible and dynamic! Thanks to OF developers.
__________________
~ Daniel WEI ------------- Boeing Research & Technology - China Beijing, China |
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May 7, 2009, 05:35 |
Totally wrong drag forces in OF
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#113 |
Member
P.A.
Join Date: Mar 2009
Location: Germany
Posts: 83
Rep Power: 17 |
Dear Foamers,
I hope this thread is still alive. I am fairly new to OpenFOAM, but have some experience with CFX. I am using OpenFOAM1.5-dev on a selfmade exercising case, which is a wedge like case but with some cells in circumferential direction (common three dimensional case in turbo machinery, I think). So it is rotationally symmetric. In the center of the wedge there is a section of a small torpedo like body. The whole is somehow similar to a piece of cake with a small bite of it taken away from the tip. :-) I am trying to calculate the steady drag force on this body section in water with a speed of about 6m/s (Re=10^7) using the simpleFoam solver, but compared to the CFX results, I get wrong results for x pressure force from OF, and I am lost now. Strange enough, all other components are fairly eqal to the CFX results. I used the same grid for the calculations. The setup is as follows (I will give only the essentials): INLET { type patch; nFaces 459; startFace 173842; } OUTLET { type patch; nFaces 459; startFace 174301; } AUSSEN // outer boundary of domain { type slip; nFaces 1071; startFace 174760; } SB1 // first patch of axial symmetric wedge { type cyclicGgi; separationOffset (0 0 0); rotationAxis (1 0 0); rotationAngle 10; shadowPatch SB2; bridgeOverlap false; nFaces 6761; startFace 175831; } SB2 // second patch of axial symmetric wedge { type cyclicGgi; separationOffset (0 0 0); rotationAxis (1 0 0); rotationAngle -10; shadowPatch SB1; bridgeOverlap false; nFaces 6761; startFace 182592; } GONDEL1 // surface patch of the body to retrieve forces of { type wall; nFaces 990; startFace 189353; } In the controlDict I use: application simpleFoam and forces by: functions ( forces { type forces; functionObjectLibs ("libforces.so"); patches (GONDEL1); rhoInf 1025.87; CofR (0 0 0); } ); In RASProperties I set: RASModel kOmegaSST; In transportProperties: transportModel Newtonian; nu nu [0 2 -1 0 0 0 0] 1.1883e-06; rho rho [1 -3 0 0 0 0 0] 1025.87; Originally, the density is not set in this file (in the tutorials), but I found this in some posting, and tried it. Anyway, it does not seem to cause any change in the results. So, in what cases is it useful to set it? Values for boundary conditions are: U: dimensions [0 1 -1 0 0 0 0]; internalField uniform (6.0923 0 0); boundaryField { INLET { type fixedValue; value uniform (6.0923 0 0); } SB1 { type cyclicGgi; } SB2 { type cyclicGgi; } OUTLET { type zeroGradient; } AUSSEN { type zeroGradient; } GONDEL1 { type fixedValue; value uniform (0 0 0); } } p: dimensions [0 2 -2 0 0 0 0]; internalField uniform 0; boundaryField { INLET { type zeroGradient; } SB1 { type cyclicGgi; } SB2 { type cyclicGgi; } OUTLET { type fixedValue; value uniform 0; } AUSSEN { type zeroGradient; } GONDEL1 { type zeroGradient; } } omega (using epsilon and k, which I calculated in the same way as is done in the user guide): dimensions [0 0 -1 0 0 0 0]; internalField uniform 0.015; boundaryField { INLET { type turbulentMixingLengthFrequencyInlet; mixingLength 4; k k; value 0.015; } ... k: dimensions [0 2 -2 0 0 0 0]; internalField uniform 0.004865; boundaryField { INLET { type fixedValue; value 0.004865; } ... RESULTS: The results from OF are (only forces): 2750 ((11.1798 152.876 13.3751) (4.76695 0.254509 0.0178232)) The results from CFX are (ordered in the same manner): 1924 ((0.77298 133.43 11.674) (3.6813 0.21366 0.018662)) The pressure distribution on the GONDEL1 patch looks very similar in CFX and OF, but the value ranges differ slightly (p, not p*): CFX: -4284 to 18850 OF: -5223 to 24892 Due to our long term experience with CFX I can almost certain exclude the possibility of a mistake in the CFX setup. I suppose I missed something very basic in OF, but I cannot figure it out. Any hint is warmly appreciated! Thanks, Pascal. |
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May 12, 2009, 05:51 |
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#114 |
Super Moderator
Maxime Perelli
Join Date: Mar 2009
Location: Switzerland
Posts: 3,297
Rep Power: 41 |
I have a question about the forces.c which generates the file forces.dat
if I plot the result vs Time in gnuplot, I am not able to see the first components of the vectors. I think gnuplot ignore those values because of the "(" Is there a workaround in gnuplot, which skip all the "("?
__________________
In memory of my friend Hervé: CFD engineer & freerider |
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May 12, 2009, 06:29 |
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#115 |
Senior Member
Wolfgang Heydlauff
Join Date: Mar 2009
Location: Germany
Posts: 136
Rep Power: 21 |
use the forceCoeffs Tool. Set v=1, A=1,63 in controlDict so the tool calculates the CL values as if there were the L values.
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May 12, 2009, 07:14 |
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#116 | |
Super Moderator
Maxime Perelli
Join Date: Mar 2009
Location: Switzerland
Posts: 3,297
Rep Power: 41 |
Quote:
So I get the pressure force at the inlet (this is the x-axis in my case ) and I divide it with the inlet-area On the other hand, the viscous effects should be negligible, so I can work with the total force, eg: the coefficients
__________________
In memory of my friend Hervé: CFD engineer & freerider Last edited by -mAx-; May 12, 2009 at 10:07. Reason: reflection |
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May 13, 2009, 03:53 |
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#117 |
Super Moderator
Maxime Perelli
Join Date: Mar 2009
Location: Switzerland
Posts: 3,297
Rep Power: 41 |
To filter the opening parenthesis in gnuplot
>plot "<sed 's/(/ /g' forces.dat" u 1:2 w l
__________________
In memory of my friend Hervé: CFD engineer & freerider |
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May 18, 2009, 05:10 |
Cannot relate answer to appropriate posting
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#118 | |
Member
P.A.
Join Date: Mar 2009
Location: Germany
Posts: 83
Rep Power: 17 |
Quote:
was this posting meant as a reply to my posting from May, 7th (don't understand the Linkback URL completely, but this is the only reference URL I can find for my posting: http://www.cfd-online.com/Forums/ope...rces-of15.html) about the wrong x forces in OF and the comparison to CFX? If this is the case, I do not understand where the A=1.63 value comes from? If this posting is a reply to mAx question about filtering of "(" in gnuplot, then I do not understand the correlation either. Please shed a little light on this. Thank you! Cheers, Pascal. |
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May 18, 2009, 05:27 |
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#119 |
Senior Member
Wolfgang Heydlauff
Join Date: Mar 2009
Location: Germany
Posts: 136
Rep Power: 21 |
Hi blaise,
was a reply to mAx post. if on a wing the lift is L = 0.5 * rho * u^2 * A * cL and you take U as 1m/s and the area A=1.63 m˛, then you get the values of cL as if they were the lift L. because 1.63 is the reciprocal of 0.5*rho ....... i think the results of the drag are calculated too high in OF (or forces-tool). I also have problems calculating an airfoil. drag is too high about 15% compared to windtunnel measurements. but the fit the calculated values of FLOWer e.g. |
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May 30, 2009, 14:25 |
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#120 |
Member
Hai Yu
Join Date: Mar 2009
Location: Harbin
Posts: 67
Rep Power: 17 |
hi ,dear foamers,
I am not sure whether the default density of liquid for turbFoam is air ? 1.29 or 1.225? if I want to specify it, I should introduce a item in turbulenceProperty "rho" following nu? thanks! Cheers |
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