5.7. Example Damped Modal Cyclic Symmetry Analysis

This example damped modal cyclic symmetry analysis presents a simplified ring-strut-ring structure used in many rotating-machinery applications.

5.7.1. Problem Description

This example is very similar to Example Modal Cyclic Symmetry Analysis, except that a damped modal analysis is performed. The component is a simplified fan inlet case for a military aircraft engine.

5.7.2. Problem Specifications

The problem specifications follow those of Example Modal Cyclic Symmetry Analysis, with the addition of alpha (mass proportional) and structural damping coefficients equal to 0.1.

5.7.3. Input File for the Analysis

! Damped Modal Cyclic Symmetry Analysis Example
! Ring-Strut-Ring Configuration

! Define constants
r1=5
r2=10
d1=2
nsect=24
alpha_deg=360/nsect
alpha_rad=2*acos(-1)/nsect

! Plot settings
/view,1,1,1,2
/plopts,minm,0
/plopts,date,0
/plopts,logo,on
/pnum,real,1
/number,1

! Create a cyclic symmetry ring-strut-ring model
/prep7
csys,1
k,1,0,0,0
k,2,0,0,d1
k,3,r1,0,0
k,4,r1,0,d1
l,3,4
arotat,1,,,,,,1,2,alpha_deg/2
k,7,r2,0,0
k,8,r2,0,d1
l,7,8
arotat,5,,,,,,1,2,alpha_deg/2
arotat,2,,,,,,1,2,alpha_deg/2
arotat,6,,,,,,1,2,alpha_deg/2
a,5,6,10,9
mshkey,1
et,1,181
r,1,0.20
r,2,0.1
mp,ex,1,10e6
mp,prxy,1,0.3
mp,dens,1,1e-4
esize,0.5
asel,,,,1,4
aatt,,1
asel,,,,5
aatt,,2
allsel
cyclic
amesh,all
finish

! Perform a damped modal solve
/solution
antype,modal
modopt,damp,6   ! Select damped eigensolver (unity norm by default)
mxpand,6,,,yes
alphad,0.1      ! Apply global alpha damping
dmpstr,0.1      ! Apply structural damping
dk,5,uz,0
solve
finish

/post1
set,list
set,list,,, ,,, ,order
/cycexpand
rsys,1

! Read results for "load step 1 - substep 3 - harmonic index 0"
! Plot the real and imaginary tangential displacement contour
set,1,3,,real
plns,u,y

set,1,3,,imag
plns,u,y

! Read results for "load step 13 - substep 1 - harmonic index 12"
! Plot the real tangential displacement contour
set,13,1,,real
plns,u,y

! Read results for "load step 3 - substep 5 - harmonic index 1"
! Plot the real and imaginary tangential displacement contour
set,3,5,,real
plns,u,y

set,3,5,,imag
plns,u,y

5.7.4. Analysis Steps

The following table describes the input listing and the steps involved in this example damped modal cyclic symmetry analysis in more detail.

Step Description Command
1.

Start an interactive session.

---

2.

Create the Ring-Strut-Ring model.

---

3.

Specify a cyclic symmetry analysis and configure the database accordingly.

CYCLIC
4.

Mesh the areas.

AMESH,ALL
5.

Specify the damped eigensolver.

MODOPT,DAMP
6.

Apply global alpha damping.

ALPHAD,0.1
7.Apply structural damping. DMPSTR,0.1
8.

Solve the modal cyclic symmetry analysis.

9.List complex eigenvalues. SET,LIST
10.

Specify the global cylindrical coordinate system.

11.

Read results for "load step 1 - substep 3 - harmonic index 0." This can be done for both real and imaginary results.

SET,1,3,,REAL
SET,1,3,,IMAG
12.

Plot the real and imaginary tangential displacement contour.

Executing this step causes the struts of the assembly to bend "in phase."

PLNSOL,U,Y
13.Read results for "load step 13 - substep 1 - harmonic index 12." SET,13,1,REAL
14.

Plot the real tangential displacement contour.

Executing this step causes the struts of the assembly to bend "out of phase."

PLNSOL,U,Y
15.

Read results for "load step 3 - substep 5 - harmonic index 1."

SET,3,5,,REAL
SET,3,5,,IMAG
16.

Plot the imaginary tangential displacement contour.

----

This step completes the example damped modal cyclic symmetry analysis.

PLNSOL,U,Y

The results of your analysis should match those shown below.

Table 5.2: Sample Complex Eigenvalues

SET TIME/FREQ LOAD STEP SUBSTEP CUMULATIVE HRM-INDEX
1-1.04E-041110
2-5.40E-051110
3-1.58E-021220
45.40E-051220
5-17.821330
6357.131330
717.8041440
8-357.131440
9-38.8351550
10778.481550
1138.8191660
12-778.481660
13-6.00E-122171
147.57E-152171
15-3.47E-052281
163.87E-062281
17-1.59E-022391
18-3.87E-062391
19-1.59E-0224101
201.63E-1724101
21-33.08925111
22663.2725111
2333.07326121
24-663.2726121
2510.16431132
26-203.9531132
2710.16432142
...... ...... ... ...

Figure 5.22: Damped Modal Cyclic Symmetry Analysis Results - Real

Damped Modal Cyclic Symmetry Analysis Results - Real

Figure 5.23: Damped Modal Cyclic Symmetry Analysis Results - Imaginary

Damped Modal Cyclic Symmetry Analysis Results - Imaginary


Note:  Mode shape values may vary slightly depending on your computer system.