4.29 FLUID29 2-D Acoustic Fluid

4.29 FLUID29 2-D Acoustic Fluid (UP19980821 ) FLUID29 is used for modeling the fluid medium and the interface in fluid/structure interaction problems. Typical applications include sound wave propagation and submerged structure dynamics. The governing equation for acoustics, namely the 2-D wave equation, has been discretized taking into account the coupling of acoustic pressure and structural motion at the interface. The element has four corner nodes with three degrees of freedom per node: translations in the nodal x and y directions and pressure. The translations, however, are applicable only at nodes that are on the interface.

The element has the capability to include damping of sound absorbing material at the interface. The element can be used with other 2-D structural elements to perform unsymmetric or damped modal, full harmonic response and full transient method analyses (see the description of the TRNOPT command). When there is no structural motion, the element is also applicable to static, modal and reduced harmonic response analyses. See Section 14.29 in the ANSYS Theory Reference for more details about this element.

Figure 4.29-1 FLUID29 2-D Acoustic Fluid



4.29.1 Input Data

The geometry, node locations, and the coordinate system for this element are shown in Figure 4.29-1. The element is defined by four nodes, a reference pressure, and the isotropic material properties. The reference pressure (PREF) is used to calculate the element sound pressure level (defaults to 20x10-6 N/m2). The speed of sound () in the fluid is input by SONC where k is the bulk modulus of the fluid (Force/Area) and is the mean fluid density (Mass/Volume) (input as DENS). The dissipative effect due to fluid viscosity is neglected, but absorption of sound at the interface is accounted for by generating a damping matrix using the surface area and boundary admittance at the interface. Experimentally measured values of the boundary admittance for the sound absorbing material may be input as material property MU (with values from 0.0 to 1.0). MU=0.0 represents no sound absorption and MU=1.0 represents full sound absorption. DENS, SONC and MU are evaluated at the average of the nodal temperatures.

Nodal flow rates, if any, may be specified using the F command where both the real and imaginary components may be applied. Nodal flow rates should be input per unit of depth for a plane analysis and on a 360° basis for an axisymmetric analysis.

Element loads are described in Section 2.7 Fluid-structure interfaces (FSI) may be flagged by surface loads at the element faces as shown by the circled numbers on Figure 4.29-1. Specifying the FSI label (without a value) [SF, SFA, SFE] will couple the structural motion and fluid pressure at the interface. Deleting the FSI specification [SFDELE, SFADELE, SFEDELE] removes the flag. The flag specification should be on the fluid elements at the interface. The surface load label IMPD with a value of unity should be used to include damping that may be present at a structural boundary with a sound absorption lining. A zero value of IMPD removes the damping calculation. The displacement degrees of freedom (UX and UY) at the element nodes not on the interface should be set to zero to avoid zero-pivot warning messages.

Temperatures may be input as element body loads at the nodes. The node I temperature T(I) defaults to TUNIF. If all other temperatures are unspecified, they default to T(I). For any other input pattern, unspecified temperatures default to TUNIF.

KEYOPT(2) is used to specify the absence of a structure at the interface and, therefore, the absence of coupling between the fluid and structure. Since the absence of coupling produces symmetric element matrices, a symmetric eigensolver [MODOPT] may be used within the modal analysis. However, for the coupled (unsymmetric) problem, a corresponding unsymmetric eigensolver [MODOPT] must be used.

A summary of the element input is given in Table 4.29-1. A general description of element input is given in Section 2.1.

Table 4.29-1 FLUID29 Input Summary

Element Name

FLUID29

Nodes

I, J, K, L

Degrees of Freedom

UX, UY, PRES if KEYOPT (2) = 0
PRES if KEYOPT (2) = 1

Real Constants

PREF

Material Properties

DENS, SONC, MU

Surface Loads

Fluid-structure Interface Flag:
face 1 (J-I), face 2 (K-J), face 3 (L-K), face 4 (I-L)
Impedance:
face 1 (J-I), face 2 (K-J), face 3 (L-K), face 4 (I-L)

Body Loads

Temperatures: T (I), T (J), T (K), T (L)

KEYOPT(2)

0 - Structure present at interface (unsymmetric element matrix)
1 - No structure at interface (symmetric element matrix)

KEYOPT(3)

0 - Planar
1 - Axisymmetric


4.29.2 Output Data

The solution output associated with the element is in two forms:

Section 2.2 gives a general description of solution output. See the ANSYS Basic Analysis Procedures Guide for ways to view results.

The following notation is used in Table 4.29-2:

A colon (:) in the Name column indicates the item can be accessed by the Component Name method [ETABLE, ESOL] (see Section 2.2.2). The O and R columns indicate the availability of the items in the file Jobname.OUT (O) or in the results file (R), a Y indicates that the item is always available, a number refers to a table footnote which describes when the item is conditionally available, and a - indicates that the item is not available.

Table 4.29-2 FLUID29 Element Output Definitions

Name

Definition

O

R

EL

Element number

Y Y
NODES

Nodes - I, J, K, L

Y Y
MAT

Material number

Y Y
VOLU:

Volume

Y Y
CENT: X, Y

Global location XC, YC

Y Y
TEMP

Temperatures T(I), T(J), T(K), T(L)

Y Y
PRESSURE

Average pressure

Y Y
PG( X, Y, SUM)

Pressure gradient components and vector sum

Y Y
VL( X, Y, SUM)

Fluid velocity components and vector sum

1 1
SOUND PR.LEVEL

Sound pressure level (in decibels)

1 1
1. Output only if ANTYPE=HARMIC

Table 4.29-3 lists output available through the ETABLE command using the Sequence Number method. See Chapter 5 of the ANSYS Basic Analysis Procedures Guide and Section 2.2.2.2 of this manual for more information. The following notation is used in Table 4.29-3:

Table 4.29-3 FLUID29 Item and Sequence Numbers for the ETABLE and ESOL Commands

Name

Item

E

PGX

SMISC

1
PGY

SMISC

2
VLX

SMISC

3
VLY

SMISC

4
PRESSURE

NMISC

1
PGSUM

NMISC

2
VLSUM

NMISC

3
SOUND PR. LEVEL

NMISC

4

4.29.3 Assumptions and Restrictions

The area of the element must be positive. The element must lie in a global X-Y plane as shown in Figure 4.29-1. All elements must have 4 nodes. A triangular element may be formed by defining duplicate K and L nodes (see Section 2.8).

The acoustic pressure in the fluid medium is determined by the wave equation with the following assumptions:

1. The fluid is compressible (density changes due to pressure variations).

2. Inviscid fluid (no dissipative effect due to viscosity).

3. There is no mean flow of the fluid.

4. The mean density and pressure are uniform throughout the fluid. Note that the acoustic pressure is the excess pressure from the mean pressure.

5. Analyses are limited to relatively small acoustic pressures so that the changes in density are small compared with the mean density.

The lumped mass matrix formulation [LUMPM,ON] is not allowed for this element.

4.29.4 Product Restrictions

There are no product-specific restrictions for this element.