Hello All
I have a shell model of a large car carrier (length = 220 metres), model consists of shell181 and beam 188 elements. I need to apply a constant unit bending moment MY over the length of the model.
At both ends of the model there are planar cross-sections which contain the necessary nodes for the moment input. I know the position of the neutral axes at these cross-sections.
I would like to apply a unit bending moment MY on one node only (at the neutral axis position per cross-section) and rotate the complete cross-section with this moment, while the cross section would stay planar (but nodes are free to move along the plane).
In effect this means that the planar end cross-sections would be rotated about their neutral axes by the unit moments.
Looking through the ANSYS commands (and xansys archive), I did not find a way to do this using coupling or constraint equations functionalities.
So the question is, if anybody has found a way to do this?
Any help is appreciated,
BR Marko
Hello! Are you doing this in Mechanical or APDL? If Mechanical, I think this could be done by assigning a Remote Displacement to the planar face. Ensure its located directly on the neutral axis of the planar face. Then specify the unit moment for the remote displacement. As far as the face remaining planar, two ideas come to mind:
If I was doing this in APDL, I cannot remember how to build remote displacements therein. Therefore, I would first build a small test model in Mechanical and then study the DS.DAT file to see how the solver built the remote displacement. Then I could reproduce it in APDL.
One last thing...You mentioned a moment on each end. I think it would be the same to fix one end and apply the moment to the other end. I'm thinking about simple beam theory from college. If one end of a beam is fixed and a moment applied to the other end, the entire beam experiences the same moment along the length.
-Matt
-----Original Message-----
From: Marko Aalto via Xansys xansys-temp@list.xansys.org
Sent: Wednesday, February 19, 2025 8:18 AM
To: xansys-temp@list.xansys.org
Cc: marko.aalto@deltamarin.com
Subject: [Xansys] [APDL] Applying planar rotation at the end of a structural model
Hello All
I have a shell model of a large car carrier (length = 220 metres), model consists of shell181 and beam 188 elements. I need to apply a constant unit bending moment MY over the length of the model.
At both ends of the model there are planar cross-sections which contain the necessary nodes for the moment input. I know the position of the neutral axes at these cross-sections.
I would like to apply a unit bending moment MY on one node only (at the neutral axis position per cross-section) and rotate the complete cross-section with this moment, while the cross section would stay planar (but nodes are free to move along the plane).
In effect this means that the planar end cross-sections would be rotated about their neutral axes by the unit moments.
Looking through the ANSYS commands (and xansys archive), I did not find a way to do this using coupling or constraint equations functionalities.
So the question is, if anybody has found a way to do this?
Any help is appreciated,
BR Marko
Xansys mailing list -- xansys-temp@list.xansys.org To unsubscribe send an email to xansys-temp-leave@list.xansys.org If you are receiving too many emails from XANSYS please consider changing account settings to Digest mode which will send a single email per day.
Please send administrative requests such as deletion from XANSYS to xansys-mod@tynecomp.co.uk and not to the list
From my experience with ANSYS, direct application of moment is not
possible. However, there are some work arounds like remembering that the
moment is the multiplication of the force by the distance (M=F.d). So, if
you know the distance from the fixed support to the load application
location, a unity moment can be equivalently defined as (F=1/d).
I hope this helps.
Best,
Mohammad
---====
Mohammad A Gharaibeh, Ph.D.
Associate Professor
Department of Mechanical Engineering
The Hashemite University
P.O. Box 330127
Zarqa, 13133, Jordan
Tel: +962 - 5 - 390 3333 Ext. 4771
Fax: +962 - 5 - 382 6348
---====
On Wed, 19 Feb 2025 at 4:19 PM Marko Aalto via Xansys <
xansys-temp@list.xansys.org> wrote:
Hello All
I have a shell model of a large car carrier (length = 220 metres), model
consists of shell181 and beam 188 elements. I need to apply a constant unit
bending moment MY over the length of the model.
At both ends of the model there are planar cross-sections which contain
the necessary nodes for the moment input. I know the position of the
neutral axes at these cross-sections.
I would like to apply a unit bending moment MY on one node only (at the
neutral axis position per cross-section) and rotate the complete
cross-section with this moment, while the cross section would stay planar
(but nodes are free to move along the plane).
In effect this means that the planar end cross-sections would be rotated
about their neutral axes by the unit moments.
Looking through the ANSYS commands (and xansys archive), I did not find a
way to do this using coupling or constraint equations functionalities.
So the question is, if anybody has found a way to do this?
Any help is appreciated,
BR Marko
Xansys mailing list -- xansys-temp@list.xansys.org
To unsubscribe send an email to xansys-temp-leave@list.xansys.org
If you are receiving too many emails from XANSYS please consider changing
account settings to Digest mode which will send a single email per day.
Please send administrative requests such as deletion from XANSYS to
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I tend to believe moment can be applied by using remote force / remote moment feature. It has been a while I looked into it and cannot recall the details. Check it out.
[Ontario Power Generation logo] Hassan Kazi
9053029636
From: Mohammad Gharaibeh via Xansys xansys-temp@list.xansys.org
Sent: Wednesday, February 19, 2025 9:22 AM
To: XANSYS Mailing List Home xansys-temp@list.xansys.org
Cc: Mohammad Gharaibeh mgharai1@binghamton.edu
Subject: [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
From my experience with ANSYS, direct application of moment is not
possible. However, there are some work arounds like remembering that the
moment is the multiplication of the force by the distance (M=F.d). So, if
you know the distance from the fixed support to the load application
location, a unity moment can be equivalently defined as (F=1/d).
I hope this helps.
Best,
Mohammad
---====
Mohammad A Gharaibeh, Ph.D.
Associate Professor
Department of Mechanical Engineering
The Hashemite University
P.O. Box 330127
Zarqa, 13133, Jordan
Tel: +962 - 5 - 390 3333 Ext. 4771
Fax: +962 - 5 - 382 6348
---====
On Wed, 19 Feb 2025 at 4:19 PM Marko Aalto via Xansys <
xansys-temp@list.xansys.org> wrote:
Hello All
I have a shell model of a large car carrier (length = 220 metres), model
consists of shell181 and beam 188 elements. I need to apply a constant unit
bending moment MY over the length of the model.
At both ends of the model there are planar cross-sections which contain
the necessary nodes for the moment input. I know the position of the
neutral axes at these cross-sections.
I would like to apply a unit bending moment MY on one node only (at the
neutral axis position per cross-section) and rotate the complete
cross-section with this moment, while the cross section would stay planar
(but nodes are free to move along the plane).
In effect this means that the planar end cross-sections would be rotated
about their neutral axes by the unit moments.
Looking through the ANSYS commands (and xansys archive), I did not find a
way to do this using coupling or constraint equations functionalities.
So the question is, if anybody has found a way to do this?
Any help is appreciated,
BR Marko
Xansys mailing list -- xansys-temp@list.xansys.org
To unsubscribe send an email to xansys-temp-leave@list.xansys.org
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THIS MESSAGE IS ONLY INTENDED FOR THE USE OF THE INTENDED RECIPIENT(S) AND MAY CONTAIN INFORMATION THAT IS PRIVILEGED, PROPRIETARY AND/OR CONFIDENTIAL. If you are not the intended recipient, you are hereby notified that any review, retransmission, dissemination, distribution, copying, conversion to hard copy or other use of this communication is strictly prohibited. If you are not the intended recipient and have received this message in error, please notify me by return e-mail and delete this message from your system. Ontario Power Generation Inc.
Check RBE3 command, hope this helps
RBE3, Master, DOF, Slaves, Wtfact
Distributes the force/moment applied at the master node to a set of slave nodes, taking into account the geometry of the slave nodes as well as weighting factors.
Matteo Carli
Lead Mechanical Engineer – Condition Based Maintenance (Lifing models, CBM Online, Finite elements modelling)
Industrial & Energy Technology - Gas Services Engineering
Baker Hughes
T +39 (0)55 423 2119 | M +39 339 562 7528
-----Original Message-----
From: KAZI Hassan -ENTENG via Xansys xansys-temp@list.xansys.org
Sent: Wednesday, February 19, 2025 3:44 PM
To: XANSYS Mailing List Home xansys-temp@list.xansys.org
Cc: KAZI Hassan -ENTENG hassan.kazi@opg.com
Subject: [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
EXTERNAL EMAIL: This email originated outside of our organization. Do not click on any links or open attachments from unexpected or unknown senders unless you can verify the content is safe.
I tend to believe moment can be applied by using remote force / remote moment feature. It has been a while I looked into it and cannot recall the details. Check it out.
[Ontario Power Generation logo] Hassan Kazi
9053029636
From: Mohammad Gharaibeh via Xansys xansys-temp@list.xansys.org
Sent: Wednesday, February 19, 2025 9:22 AM
To: XANSYS Mailing List Home xansys-temp@list.xansys.org
Cc: Mohammad Gharaibeh mgharai1@binghamton.edu
Subject: [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
From my experience with ANSYS, direct application of moment is not possible. However, there are some work arounds like remembering that the moment is the multiplication of the force by the distance (M=F.d). So, if you know the distance from the fixed support to the load application location, a unity moment can be equivalently defined as (F=1/d).
I hope this helps.
Best,
Mohammad
---====
Mohammad A Gharaibeh, Ph.D.
Associate Professor
Department of Mechanical Engineering
The Hashemite University
P.O. Box 330127
Zarqa, 13133, Jordan
Tel: +962 - 5 - 390 3333 Ext. 4771
Fax: +962 - 5 - 382 6348
---====
On Wed, 19 Feb 2025 at 4:19 PM Marko Aalto via Xansys < xansys-temp@list.xansys.org> wrote:
Hello All
I have a shell model of a large car carrier (length = 220 metres),
model consists of shell181 and beam 188 elements. I need to apply a
constant unit bending moment MY over the length of the model.
At both ends of the model there are planar cross-sections which
contain the necessary nodes for the moment input. I know the position
of the neutral axes at these cross-sections.
I would like to apply a unit bending moment MY on one node only (at
the neutral axis position per cross-section) and rotate the complete
cross-section with this moment, while the cross section would stay
planar (but nodes are free to move along the plane).
In effect this means that the planar end cross-sections would be
rotated about their neutral axes by the unit moments.
Looking through the ANSYS commands (and xansys archive), I did not
find a way to do this using coupling or constraint equations functionalities.
So the question is, if anybody has found a way to do this?
Any help is appreciated,
BR Marko
Xansys mailing list -- xansys-temp@list.xansys.org To unsubscribe send
an email to xansys-temp-leave@list.xansys.org If you are receiving too
many emails from XANSYS please consider changing account settings to
Digest mode which will send a single email per day.
Please send administrative requests such as deletion from XANSYS to
xansys-mod@tynecomp.co.uk and not to the list
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Please send administrative requests such as deletion from XANSYS to xansys-mod@tynecomp.co.uk and not to the list
THIS MESSAGE IS ONLY INTENDED FOR THE USE OF THE INTENDED RECIPIENT(S) AND MAY CONTAIN INFORMATION THAT IS PRIVILEGED, PROPRIETARY AND/OR CONFIDENTIAL. If you are not the intended recipient, you are hereby notified that any review, retransmission, dissemination, distribution, copying, conversion to hard copy or other use of this communication is strictly prohibited. If you are not the intended recipient and have received this message in error, please notify me by return e-mail and delete this message from your system. Ontario Power Generation Inc.
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Moment is applicable to one node by F command, and distributed to other nodes by using RBE3 command, as previously suggested, or CERIG, or rigid wheel.
David Galindo
Chief Executive
PHAREA
+33 (0)4 37 66 11 40
-----Message d'origine-----
De : Carli, Matteo via Xansys xansys-temp@list.xansys.org
Envoyé : mercredi 19 février 2025 15:59
À : XANSYS Mailing List Home xansys-temp@list.xansys.org
Cc : Carli, Matteo matteo.carli@bakerhughes.com
Objet : [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
Check RBE3 command, hope this helps
RBE3, Master, DOF, Slaves, Wtfact
Distributes the force/moment applied at the master node to a set of slave nodes, taking into account the geometry of the slave nodes as well as weighting factors.
Matteo Carli
Lead Mechanical Engineer – Condition Based Maintenance (Lifing models, CBM Online, Finite elements modelling) Industrial & Energy Technology - Gas Services Engineering Baker Hughes
T +39 (0)55 423 2119 | M +39 339 562 7528
-----Original Message-----
From: KAZI Hassan -ENTENG via Xansys xansys-temp@list.xansys.org
Sent: Wednesday, February 19, 2025 3:44 PM
To: XANSYS Mailing List Home xansys-temp@list.xansys.org
Cc: KAZI Hassan -ENTENG hassan.kazi@opg.com
Subject: [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
EXTERNAL EMAIL: This email originated outside of our organization. Do not click on any links or open attachments from unexpected or unknown senders unless you can verify the content is safe.
I tend to believe moment can be applied by using remote force / remote moment feature. It has been a while I looked into it and cannot recall the details. Check it out.
[Ontario Power Generation logo] Hassan Kazi
9053029636
From: Mohammad Gharaibeh via Xansys xansys-temp@list.xansys.org
Sent: Wednesday, February 19, 2025 9:22 AM
To: XANSYS Mailing List Home xansys-temp@list.xansys.org
Cc: Mohammad Gharaibeh mgharai1@binghamton.edu
Subject: [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
From my experience with ANSYS, direct application of moment is not possible. However, there are some work arounds like remembering that the moment is the multiplication of the force by the distance (M=F.d). So, if you know the distance from the fixed support to the load application location, a unity moment can be equivalently defined as (F=1/d).
I hope this helps.
Best,
Mohammad
---====
Mohammad A Gharaibeh, Ph.D.
Associate Professor
Department of Mechanical Engineering
The Hashemite University
P.O. Box 330127
Zarqa, 13133, Jordan
Tel: +962 - 5 - 390 3333 Ext. 4771
Fax: +962 - 5 - 382 6348
---====
On Wed, 19 Feb 2025 at 4:19 PM Marko Aalto via Xansys < xansys-temp@list.xansys.org> wrote:
Hello All
I have a shell model of a large car carrier (length = 220 metres),
model consists of shell181 and beam 188 elements. I need to apply a
constant unit bending moment MY over the length of the model.
At both ends of the model there are planar cross-sections which
contain the necessary nodes for the moment input. I know the position
of the neutral axes at these cross-sections.
I would like to apply a unit bending moment MY on one node only (at
the neutral axis position per cross-section) and rotate the complete
cross-section with this moment, while the cross section would stay
planar (but nodes are free to move along the plane).
In effect this means that the planar end cross-sections would be
rotated about their neutral axes by the unit moments.
Looking through the ANSYS commands (and xansys archive), I did not
find a way to do this using coupling or constraint equations functionalities.
So the question is, if anybody has found a way to do this?
Any help is appreciated,
BR Marko
Xansys mailing list -- xansys-temp@list.xansys.org To unsubscribe send
an email to xansys-temp-leave@list.xansys.org If you are receiving too
many emails from XANSYS please consider changing account settings to
Digest mode which will send a single email per day.
Please send administrative requests such as deletion from XANSYS to
xansys-mod@tynecomp.co.uk and not to the list
Xansys mailing list -- xansys-temp@list.xansys.org To unsubscribe send an email to xansys-temp-leave@list.xansys.org If you are receiving too many emails from XANSYS please consider changing account settings to Digest mode which will send a single email per day.
Please send administrative requests such as deletion from XANSYS to xansys-mod@tynecomp.co.uk and not to the list
THIS MESSAGE IS ONLY INTENDED FOR THE USE OF THE INTENDED RECIPIENT(S) AND MAY CONTAIN INFORMATION THAT IS PRIVILEGED, PROPRIETARY AND/OR CONFIDENTIAL. If you are not the intended recipient, you are hereby notified that any review, retransmission, dissemination, distribution, copying, conversion to hard copy or other use of this communication is strictly prohibited. If you are not the intended recipient and have received this message in error, please notify me by return e-mail and delete this message from your system. Ontario Power Generation Inc.
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Please send administrative requests such as deletion from XANSYS to xansys-mod@tynecomp.co.uk and not to the list _______________________________________________
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The RBE3 seems the command I need here, thank you very much!
Need to experiment with it though once I have more time for that, first results I got show local deformation at/near the independent node which should not be there if the complete cross-section is rotated by a plane.
Concerning one reply where it was mentioned that fixing the other end DOF would do the same as applying moments at both ends…I believe that if other end fixed like a cantilever beam then there will be a reaction force + moment at the fixed end - and I want to have a ‘pure’ bending moment without the shear force.
Thank you All!
Marko Aalto, M.Sc.
Project Discipline Manager, Hull FEA & Rule calculations
Deltamarin Ltd, Postikatu 2, FI-20250 Turku, Finland, www.deltamarin.com
Tel. +358 40 7648098
"I believe that if other end fixed like a cantilever beam then there will be a reaction force + moment at the fixed end - and I want to have a ‘pure’ bending moment without the shear force."
There should be no shear force whatsoever, anywhere in the beam including the fixed end, if the beam is loaded with a pure moment at the cantilevered end. A shear/moment diagram from beam statics would reveal this.
Nevertheless, best of luck. Keep us updated on your progress! ;-)
—Matt
-----Original Message-----
From: Marko Aalto via Xansys xansys-temp@list.xansys.org
Sent: Thursday, February 20, 2025 8:25 AM
To: xansys-temp@list.xansys.org
Cc: marko.aalto@deltamarin.com
Subject: [Xansys] Re: [External Email] [APDL] Applying planar rotation at the end of a structural model
The RBE3 seems the command I need here, thank you very much!
Need to experiment with it though once I have more time for that, first results I got show local deformation at/near the independent node which should not be there if the complete cross-section is rotated by a plane.
Concerning one reply where it was mentioned that fixing the other end DOF would do the same as applying moments at both ends…I believe that if other end fixed like a cantilever beam then there will be a reaction force + moment at the fixed end - and I want to have a ‘pure’ bending moment without the shear force.
Thank you All!
Marko Aalto, M.Sc.
Project Discipline Manager, Hull FEA & Rule calculations
Deltamarin Ltd, Postikatu 2, FI-20250 Turku, Finland, www.deltamarin.com
Tel. +358 40 7648098
Xansys mailing list -- xansys-temp@list.xansys.org To unsubscribe send an email to xansys-temp-leave@list.xansys.org If you are receiving too many emails from XANSYS please consider changing account settings to Digest mode which will send a single email per day.
Please send administrative requests such as deletion from XANSYS to xansys-mod@tynecomp.co.uk and not to the list
Matt, yes you are right, there would be no reaction force at the fixed end, just checked this from the textbook.
- Marko
Now got the constant moment model working for a simple prismatic model, below commands listing.
Next task is to reverse the moment direction in one end to produce a constant shear force. If I just reverse the moment direction in this same listing then there will be deformation at the location of the ‘independent’ nodes where the reaction forces are developed.
Need to experiment with the RBE3 dof to see if this can be fixed. If anyone knows a trick how to keep the end sections undeformed pls let me know,
-Marko
FINISH
/CLEAR
/PREP7
K,,0,0,0
,,0,1000,0
,,0,2000,0
KGEN,3,1,3,1,0,0,2500
L,1,2
,2,3
,4,5
,5,6
,7,8
,8,9
,1,4
,4,7
,2,5
,5,8
,3,6
,6,9
LGEN,2,1,12,1,20000,0,0
A,1,2,11,10
,2,3,12,11
,4,5,14,13
,5,6,15,14
,7,8,17,16
,8,9,18,17
,1,4,13,10
,4,7,16,13
,3,6,15,12
,6,9,18,15
!,2,5,14,11
!*,5,8,17,14
ET,1,181
SECTYPE,,SHELL
SECDATA,10
MPTEMP,,,,,,,,
MPTEMP,1,0
MPDATA,EX,1,,206000
MPDATA,PRXY,1,,.3
AESIZE,ALL,500
NKPT,,ALL
AMESH,ALL
NUMMRG,ALL,ALL
!* Aft end
N_AFT=5
N_FORE=14
NSEL,S,LOC,X,0
RBE3,N_AFT,ROTY,ALL
!* Fore end
ALLSEL,ALL
NSEL,S,LOC,X,20000
RBE3,N_FORE,ROTY,ALL
!* Loads - Unit moments MY
ALLSEL,ALL
D,N_AFT,UX,0
D,N_AFT,UY,0
D,N_AFT,UZ,0
!*,N_AFT,ROTX,0
!*,N_FORE,UY,0
D,N_FORE,UZ,0
F,N_AFT,MY,1000
F,N_FORE,MY,-1000
LSWRITE,1
FINI
/SOLU
SOLVE
FINI
/POST1
SET,1
/VIEW,1,,1
/ANG,1
/PBC,M,,2
/PBC,NFOR,,1
PLDI,1