PIPE18


Elastic Curved Pipe

Valid Products: Pro | Premium | Enterprise | PrepPost | Solver | AS add-on

PIPE18 Element Description

Although this archived element is available for use in your analysis, Ansys, Inc. recommends using a current-technology element such as ELBOW290.

PIPE18, also known as an elbow element, is a circularly uniaxial element with tension, compression, torsion, and bending capabilities. The element has six degrees of freedom at each node: translations in the nodal x, y, and z directions and rotations about the nodal x, y, and z axes.

Options are available to include various flexibility and stress intensification factors in the formulation. The element can account for insulation, contained fluid, and a corrosion allowance. See PIPE18 - Elastic Curved Pipe for more details about this element.

Figure 18.1: PIPE18 Geometry

PIPE18 Geometry

PIPE18 Input Data

The geometry, node locations, and the coordinate system for this element are shown in Figure 18.1: PIPE18 Geometry. The element input data include three nodes, the pipe outer diameter, wall thickness, radius of curvature, optional stress intensification and flexibility factors, internal fluid density, exterior insulation density and thickness, corrosion thickness allowance, and the isotropic material properties. The internal fluid and external insulation constants are used only to determine the added mass effects for these components.

Although the curved pipe element has only two endpoints (nodes I and J), the third node (K) is required to define the plane in which the element lies. This node must lie in the plane of the curved pipe and on the center-of-curvature side of line I-J. A node point belonging to another element (such as the other node of a connecting straight pipe element) may be used. Input and output locations around the pipe circumference identified as being at 0° are located along the element y-axis, and similarly 90° is along the element z-axis.

Only the lumped mass matrix is available.

The flexibility and stress intensification factors included in the element are calculated as follows:

Mechanical APDL Flexibility Factor = 1.65/(h(1 + PrXk/tE)) or 1.0 (whichever is greater) (used if KEYOPT(3) = 0 or 1 and FLXI not input)

Karman Flexibility Factor = (10 + 12h2)/(1 + 12h2) (used if KEYOPT(3) = 2 and FLXI not input)

User Defined Flexibility Factors = FLXI (in-plane) and FLXO (out-of-plane) (may be input as any positive value)

FLXO defaults to FLXI for all cases.

Stress Intensification Factor = 0.9/h2/3 or 1.0 (whichever is greater) (used for SIFI or SIFJ if factor not input or if input less than 1.0 (must be positive))

where:

h = tR/r2
t = thickness
R = radius of curvature
r = average radius
E = modulus of elasticity
Xk = 6 (r/t)4/3 (R/r)1/3 if KEYOPT(3) = 1 and R/r 1.7, otherwise Xk = 0
P = Pi - Po if Pi - Po > 0, otherwise P = 0, Pi = internal pressure, Po = external pressure

Do not use KEYOPT(3) = 1 if the included angle of the complete elbow is less than 360/(π(R/r)) degrees.

Element loads are described in Element Loading. Pressures may be input as surface loads on the element faces as shown by the circled numbers on Figure 18.1: PIPE18 Geometry. Internal pressure (PINT) and external pressure (POUT) are input as positive values. The internal and external pressure loads are designed for closed-loop static pressure environments and therefore include pressure loads on fictitious "end caps" so that the pressure loads induce an axial stress and/or reaction in the pipe system. If a dynamic situation needs to be represented, such as a pipe venting to a lower pressure area or the internal flow is past a constriction in the pipe, these end cap loads may need to be modified by applying a nodal force normal to the cross-section of the pipe with the magnitude representing the change in pressure. Alternatively, the precomputed end cap loads can be removed using KEYOPT(8) = 1 and the appropriate end cap loads added by the user. Note that when using KEYOPT(8) = 1, the pressure load will be acting on only the wall of the elbow element so that the total pressure load will not be self-equilibrating. The transverse pressures (PX, PY, and PZ) may represent wind or drag loads (per unit length of the pipe) and are defined in the global Cartesian directions. Positive transverse pressures act in the positive coordinate directions. Tapered pressures are not recognized. Only constant pressures are supported for this element.

Temperatures may be input as element body loads at the nodes. Temperatures may have wall gradients or diametral gradients (KEYOPT(1)). The average wall temperature at θ = 0° is computed as 2 * TAVG - T(180) and the average wall temperature at θ = -90° is computed as 2 * TAVG - T(90). The element temperatures are assumed to be linear along the length. The first temperature at node I (TOUT(I) or TAVG(I)) defaults to TUNIF. If all temperatures after the first are unspecified, they default to the first. If all temperatures at node I are input, and all temperatures at node J are unspecified, the node J temperatures default to the corresponding node I temperatures. For any other pattern of input temperatures, unspecified temperatures default to TUNIF.

For piping analyses, the PIPE module of PREP7 may be used to generate the input for this element.

A summary of the element input is given below. A general description of element input is given in Element Input.

PIPE18 Input Summary

Nodes

I, J, K - where node K is in the plane of the elbow, on the center of curvature side of line I-J

Degrees of Freedom

UX, UY, UZ, ROTX, ROTY, ROTZ

Real Constants
OD, TKWALL, RADCUR, SIFI, SIFJ, FLXI,
DENSFL, DENSIN, TKIN, TKCORR, (Blank), FLXO
See Table 18.1: PIPE18 Real Constants for a description of the real constants
Material Properties

EX, ALPX (or CTEX or THSX), PRXY (or NUXY), DENS, GXY, ALPD, BETD, DMPR

Surface Loads
Pressures -- 

1-PINT, 2-PX, 3-PY, 4-PZ, 5-POUT

Body Loads
Temperatures -- 
TOUT(I), TIN(I), TOUT(J), TIN(J) if KEYOPT (1) = 0, or
TAVG(I), T90(I), T180(I), TAVG(J), T90(J), T180(J) if KEYOPT (1) = 1
Special Features
Large deflection
Birth and death
KEYOPT(1)

Temperatures represent:

0 -- 

The through-wall gradient

1 -- 

The diametral gradient

KEYOPT(3)

Flex factor (if FLEX is not specified):

0 -- 

Use Mechanical APDL flexibility factor (without pressure term)

1 -- 

Use Mechanical APDL flexibility factor (with pressure term)

2 -- 

Use KARMAN flexibility factor

KEYOPT(6)

Member force and moment output:

0 -- 

Do not print member forces or moments

2 -- 

Print member forces and moments in the element coordinate system

KEYOPT(8)

End cap loads:

0 -- 

Internal and external pressures cause loads on end caps

1 -- 

Internal and external pressures do not cause loads on end caps

Table 18.1: PIPE18 Real Constants

No.NameDescription
1ODPipe outer diameter
2TKWALLWall thickness
3RADCURRadius of curvature
4SIFIStress intensification factor (node I)
5SIFJStress intensification factor (node J)
6FLXIFlexibility factor (in-plane)
7DENSFLInternal fluid density
8DENSINExterior insulation density
9TKINInsulation thickness
10TKCORRCorrosion thickness allowance
11(Blank)--
12FLXOFlexibility factor (out-of-plane). FLXO defaults to FLXI in all cases.

PIPE18 Output Data

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

Several items are illustrated in Figure 18.2: PIPE18 Stress Output.

The stresses are computed with the outer diameter of the pipe reduced by twice the corrosion thickness allowance. The direct stress includes the internal pressure (closed end) effect. Also printed for each end are the maximum and minimum principal stresses and the stress intensity. These quantities are computed at the outer surface and may not occur at the same location around the pipe circumference. Some of these stresses are shown in Figure 18.2: PIPE18 Stress Output. The direct stress does not include the axial component of the transverse thermal stress. The principal stresses and the stress intensity include the shear force stress component. Angles listed in the output are measured (θ) as shown in Figure 18.2: PIPE18 Stress Output. A general description of solution output is given in Solution Output. See the Basic Analysis Guide for ways to view results.

Figure 18.2: PIPE18 Stress Output

PIPE18 Stress Output

The Element Output Definitions table uses the following notation:

A colon (:) in the Name column indicates that the item can be accessed by the Component Name method (ETABLE, ESOL). The O column indicates the availability of the items in the file jobname.out. The R column indicates the availability of the items in the results file.

In either the O or R columns, “Y” indicates that the item is always available, a letter or number refers to a table footnote that describes when the item is conditionally available, and “-” indicates that the item is not available.

Table 18.2: PIPE18 Element Output Definitions

NameDefinitionOR
ELElement NumberYY
NODESNodes - I, JYY
MATMaterial numberYY
VOLU:Volume-Y
XC, YC, ZCLocation where results are reportedY 6
CORALCorrosion thickness allowance 1 1
TEMPTOUT(I), TIN(I), TOUT(J), TIN(J) 2 2
TEMPTAVG(I), T90(I), T180(I), TAVG(J), T90(J), T180(J) 3 3
PRESPINT, PX, PY, PZ, POUTYY
FFACTElement flexibility factor-Y
MFOR(X, Y, Z)Member forces for nodes I and J (in the element coordinate system) 4 Y
MMOM(X, Y, Z)Member moments for nodes I and J (in the element coordinate system) 4 Y
SFACTI, SFACTJStress intensification factors at nodes I and JYY
STHStress due to maximum thermal gradient through the wall thicknessYY
SPR2Hoop pressure stress for code calculations-Y
SMI, SMJMoment stress at nodes I and J for code calculations-Y
SDIRDirect (axial) stress-Y
SBENDMaximum bending stress at outer surface-Y
STShear stress at outer surface due to torsion-Y
SSFShear stress due to shear force-Y
S(1MX, 3MN,INTMX, EQVMX)Maximum principal stress, minimum principal stress, maximum stress intensity, maximum equivalent stress (over eight points on the outside surface at both ends of the element)YY
S(1, 3, INT, EQV)Maximum principal stress, minimum principal stress, stress intensity, equivalent stress 5 5
S(AXL, RAD, H, XH)Axial, radial, hoop, and shear stresses 5 5
EPEL(AXL, RAD, H, XH)Axial, radial, hoop, and shear strains 5 5
EPTH(AXL, RAD, H)Axial, radial, and hoop thermal strain 5 5

  1. If the value is greater than 0.

  2. If KEYOPT(1) = 0

  3. If KEYOPT(1) = 1

  4. If KEYOPT(6) = 2

  5. The item repeats at 0°, 45°, 90°, 135°, 180°, 225°, 270°, 315° at node I, then at node J (all at the outer surface)

  6. Available only at centroid as a *GET item.

The following tables list output available through the ETABLE command using the Sequence Number method. See The General Postprocessor (POST1) in the Basic Analysis Guide and The Item and Sequence Number Table of this manual for more information. The following notation is used in Table 18.3: PIPE18 Item and Sequence Numbers (Node I) through Table 18.5: PIPE18 Item and Sequence Numbers:

Name

output quantity as defined in the Table 18.2: PIPE18 Element Output Definitions

Item

predetermined Item label for ETABLE command

E

sequence number for single-valued or constant element data

I,J

sequence number for data at nodes I and J

Table 18.3: PIPE18 Item and Sequence Numbers (Node I)

Output Quantity Name ETABLE and ESOL Command Input
ItemECircumferential Location
45°90°135°180°225°270°315°
SAXLLS-1591317212529
SRADLS-26101418222630
SHLS-37111519232731
SXHLS-48121620242832
EPELAXLLEPEL-1591317212529
EPELRADLEPEL-26101418222630
EPELHLEPEL-37111519232731
EPELXHLEPEL-48121620242832
EPTHAXLLEPTH-1591317212529
EPTHRADLEPTH-26101418222630
EPTHHLEPTH-37111519232731
S1NMISC-16111621263136
S3NMISC-38131823283338
SINTNMISC-49141924293439
SEQVNMISC-510152025303540
SBENDNMISC91--------
SSFNMISC92--------
MFORXSMISC1--------
MFORYSMISC2--------
MFORZSMISC3--------
MMOMXSMISC4--------
MMOMYSMISC5--------
MMOMZSMISC6--------
SDIRSMISC13--------
STSMISC14--------
TOUTLBFE-4-1-2-3-
TINLBFE-8-5-6-7-

Table 18.4: PIPE18 Item and Sequence Numbers (Node J)

Output Quantity Name ETABLE and ESOL Command Input
ItemECircumferential Location
45°90°135°180°225°270°315°
SAXLLS-3337414549535761
SRADLS-3438424650545862
SHLS-3539434751555963
SXHLS-3640444852566064
EPELAXLLEPEL-3337414549535761
EPELRADLEPEL-3438424650545862
EPELHLEPEL-3539434751555963
EPELXHLEPEL-3640444852566064
EPTHAXLLEPTH-3337414549535761
EPTHRADLEPTH-3438424650545862
EPTHHLEPTH-3539434751555963
S1NMISC-4146515661667176
S3NMISC-4348535863687378
SINTNMISC-4449545964697479
SEQVNMISC-4550556065707580
SBENDNMISC93--------
SSFNMISC94--------
MFORXSMISC7--------
MFORYSMISC8--------
MFORZSMISC9--------
MMOMXSMISC10--------
MMOMYSMISC11--------
MMOMZSMISC12--------
SDIRSMISC15--------
STSMISC16--------
TOUTLBFE-12-9-10-11-
TINLBFE-16-13-14-15-

Table 18.5: PIPE18 Item and Sequence Numbers

Output Quantity Name ETABLE and ESOL Command Input
ItemE
SFACTINMISC81
SFACTJNMISC82
SPR2NMISC83
SMINMISC84
SMJNMISC85
S1MXNMISC86
S3MNNMISC87
SINTMXNMISC88
SEQVMXNMISC89
FFACTNMISC90
STHSMISC17
PINTSMISC18
PXSMISC19
PYSMISC20
PZSMISC21
POUTSMISC22

PIPE18 Assumptions and Restrictions

  • The curved pipe must not have a zero length or wall thickness. In addition, the OD must not be less than or equal to zero and the ID must not be less than zero.

  • The corrosion allowance must be less than the wall thickness.

  • The element is limited to having an axis with a single curvature and a subtended angle of 0° < θ  90°.

  • Shear deflection capability is also included in the element formulation.

  • The elbow is assumed to have "closed ends" so that the axial pressure effect is included.

  • When used in a large deflection analysis, the location of the third node (K) is used only to initially orient the element.

  • The element temperatures are assumed to be linear along the length. The average wall temperature at θ = 0° is computed as 2 * TAVG - T(180) and the average wall temperature at θ = -90° is computed as 2 * TAVG - T(90).

  • Stress intensification factors input with values less than 1.0 are set to 1.0.

  • The element formulation is based upon thin-walled theory. The elbow should have a large radius-to-thickness ratio since the integration points are assumed to be located at the midthickness of the wall.

  • Only the lumped mass matrix is available.

PIPE18 Product Restrictions

When used in the product(s) listed below, the stated product-specific restrictions apply to this element in addition to the general assumptions and restrictions given in the previous section.

Ansys Professional  —  

  • The ALPD and BETD material properties are not allowed.

  • The only special feature allowed is large deflection.