Dear Somayeh,
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You might look at these features:
http://lsdyna-china.com/u/b1101b1e-707e-4983-9f64-894861bc37ab/file/637092603974782368.pdf
https://ftp.lstc.com/anonymous/outgoing/hao/cbis/manuals/CONSTRAINED_SOLID_IN_SOLID.pdf
https://ftp.lstc.com/anonymous/outgoing/hao/cbis/manuals/CONSTRAINED_BEAM_IN_SOLID.pdf
https://ftp.lstc.com/anonymous/outgoing/hao/cbis/
http://lsdyna.com.cn/2017conf/document/2017_Session_Chenhao02.pdf
Chen, H., “An Introduction to *CONSTRAINED_BEAM_IN_SOLID”, FEA Information Solutions, Vol. 5, Issue 10. pp. 79-83, October, 2016.
http://www.feaiej.com/2017/feaiej_q1_2017.pdf
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A short note that might be of interest:
Moharrami, M., Chen, H., and Koutromanos, Y., “Accounting for Bond-Slip Effect in
LS-DYNA using Constrained Beam in Solid Formulation”, June, 2016.
https://ftp.lstc.com/anonymous/outgoing/hao/cbis/tutorials/presentation-Hao-Bond_slip.pdf
The assumption of a perfect-bond between concrete and steel was the first bond interaction
system studied, utilizing the *CONSTRAINED_LAGRANGE_IN_SOLID formulation.
Beam bond was another bond interaction system investigated using the *CONSTRAINED_
BEAM_IN_SOLID formulation in the program:
Iwalekar, A.A., "Finite Element Analysis and Experimental Validation of Reinforced Concrete
Single-Mat Slabs Subjected to Blast Loads", Master’s Thesis, Department of Civil and Mechanical
Engineering University of Missouri-Kansas City, Kansas City, Missouri, 2018.
https://mospace.umsystem.edu/xmlui/bitstream/handle/10355/67037/Thesis_2018_Iwalekar.pdf
The *CONSTRAINED_BEAM_IN_SOLID keyword addressed both perfect bond and
bond-slip interaction:
Lockhart, E., "Modelling the Failure of Reinforced Concrete Subjected to Dynamic
Loading Using CDPM2 in LS-DYNA", Senior Project, School of Engineering, University
of Glasgow, United Kingdom, January, 2017.
https://petergrassl.com/tempFiles/Loc17.pdf
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Examples of rebar coupled to concrete (*clis and *cbis) are given here:
http://ftp.lstc.com/anonymous/outgoing/support/FAQ_kw/concrete/coupling_by_clis.k.gz and
http://ftp.lstc.com/anonymous/outgoing/support/FAQ_kw/concrete/coupling_by_cbis.k.gz
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Sincerely,
James M. Kennedy
KBS2 Inc.
April 14, 2021
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Dear Somayeh,
Please see if the intermittent eigenvalue analysis is of some help.
From the LS-DYNA User’s Manual:
http://ftp.lstc.com/anonymous/outgoing/jday/manuals/DRAFT_Vol_I.pdf
*CONTROL_IMPLICIT_EIGENVALUE
Remarks:
1. Performing Eigenvalue Analysis. To perform an eigenvalue analysis, activate
the implicit method by selecting IMFLAG = 1 on *CONTROL_IMPLICIT_-
GENERAL, and indicate a nonzero value for NEIG above. By default, the lowest
NEIG eigenvalues will be found. If a nonzero center frequency is specified, the
NEIG eigenvalues nearest to CENTER will be found.
When NEIG > 0, eigenvalues will be computed at time = 0 and LS-DYNA will
terminate.
When NEIG < 0, an intermittent eigenvalue analysis will be performed. This is a
transient simulation during which loads are applied, with eigenvalues computed
periodically during the simulation. Changes in geometry, stress, material, and
contact conditions will affect the eigenvalues. The transient simulation can be
either implicit or explicit according to IMFLAG = 1 or IMFLAG = 6, respectively,
on *CONTROL_IMPLICIT_GENERAL. The curve ID = -NEIG indicates when
to extract eigenvalues, and how many to extract. Define one curve point at each
desired extraction time, with a function value equal to the number of eigenvalues
desired at that time. A d3plot database will be produced for the transient solution
results. Consecutively numbered d3eigv and eigout databases will be produced
for each intermittent extraction. The extraction time is indicated in each database’s
analysis title.
Sincerely,
James M. Kennedy
KBS2 Inc.
April 15, 2021
To view this discussion on the web visit https://groups.google.com/d/msgid/ls-dyna2/431aaafc-50b9-4476-92c2-22f876f79c5fn%40googlegroups.com.
Dear Somayeh,
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http://www.d3view.com/dynamic-solution-type-using-imflag-in-control_implicit_general/
3. Intermittent Eigenvalue Extration, IMFLAG = 6.
For IMFLAG=6, LS-DYNA uses Explicit and allows the extraction of eigenvalues
intermittently throughout the simulation. To define the times at which the eigenvalue
extraction is performed, the parameter NEIGV in *CONTROL_IMPLICIT_
EIGENVALUE must be set to a negative number. The absolute value of NEIGV
then refers to a load curve ID (see LCID in *DEFINE_CURVE) which allows the
user to define the number of eigenvalues as a function of simulation time. It should
be noted that the abscissa axis refers to time that can be either pseudo or transient
beginning in LS-DYNA version 971R3 allowing users to extract eigenvalues even
in the dynamic relaxation phase. Negative abscissa values correspond to pseudo time,
and positive values correspond to the transient portion of the simulation. It is also
important to note that a user can extract intermittent eigenvalues during the Implicit
solution by setting IMFLAG=1 and using a negative value for NEIGV. In versions
prior to 971R3, the abscissa points were not treated as key-points such that the
Implicit timestep is automatically adjusted to meet the time specified in NEIGV
curve. For example, if DT0=0.2 and the current converged step is at 1.0 seconds,
then an abscissa point in NEIGV of 1.1 will be skipped without any eigenvalue
extraction. To force the implicit solver to auto-adjust the timestep such that the
abscissa time point in NEIGV is met, it is recommended that the parameter DTMAX
in *CONTROL_IMPLICIT_AUTO is used. However, in versions 971R3 and higher,
the points specified in NEIGV will be treated as key points and the solver will auto-
adjust the timestep to solve at the points and extract the eigenvalues. A sample curve
for intermittent eigenvalue extraction using NEIGV is shown in the following figure:
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As I understand it, there is no special theory for intermittent eigenvalue analysis.
It is basically using the theory of general eigenvalue analysis. Perhaps the following
report might offer some help:
Chowdhury, M.R., and Tabiei, A., "Development of an Air Gun Simulation Model
Using LS-DYNA", Report ARL-TR-3016, U.S. Army Research Laboratory,
Aberdeen Proving Grounds, Maryland, July, 2003.
http://www.arl.army.mil/arlreports/2003/ARL-TR-3016.pdf
2.2.6 Intermittent Eigenvalues Analysis
To understand the frequency content in this simulation, an intermittent eigenvalue
analysis is conducted. The LS-DYNA code allows for the extraction of frequency
contents during an impact simulation. This is performed to relate the frequency
content to the event and deformation mode in the OBR. The FFT of the unfiltered
acceleration of the OBR is depicted in figure 36. One can see several important
peaks in the data. The largest peak corresponds to the first fundamental mode. The
next peak is at about 7400 Hz. The next ones are at about 8000, 14600, 21000, 23800,
27700, and 29500 Hz. The intermittent eigenvalue analysis revealed the sources of
these frequencies. One hundred modes were extracted from the analysis.
-------------------------------------------------
Sincerely,
James M. Kennedy
KBS2 Inc.
April 15, 2021
Sincerely,
James M. Kennedy
KBS2 Inc.
April 15, 2021
To view this discussion on the web visit https://groups.google.com/d/msgid/ls-dyna2/431aaafc-50b9-4476-92c2-22f876f79c5fn%40googlegroups.com.
Dear Somayeh,
Several presentations perhaps of interest:
Li, L., and Grimes, R., "Introduction of Rotor Dynamics Using Implicit Method
in LS-DYNA", 13th International LS-DYNA Users Conference, Dearborn, Michigan,
June, 2014.
Li, L., Grimes, R., and Borrvall, T. "Introduction of Rotor Dynamics Using Implicit
Method in LS-DYNA", 14th International LS-DYNA Users Conference, Dearborn, Michigan,
June, 2016.
Sincerely,
James M. Kennedy
KBS2 Inc.
April 15, 2021
To view this discussion on the web visit https://groups.google.com/d/msgid/ls-dyna2/00fd01d73224%24e085de40%24a1919ac0%24%40kbs2.com.