4.17 PIPE17 Elastic Pipe Tee

4.17 PIPE17 Elastic Pipe Tee (UP19980821 ) PIPE17 is a combination of three uniaxial elastic straight pipe elements (PIPE16) arranged in a "tee" configuration, 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 tee-joint flexibility and stress intensification factors and to print member forces. The element can account for insulation, contained fluid, and a corrosion allowance. See Section 14.17 in the ANSYS Theory Reference for more details about this element.

The I and J nomenclature used in the description of this element refers to the first and second end of each branch of the element, i.e., I-J for branch 1, J-K for branch 2, and J-L for branch 3.

Figure 4.17-1 PIPE17 Elastic Pipe Tee



4.17.1 Input Data

The geometry, node locations, and the coordinate system for this element are shown in Figure 4.17-1. The element input data include four nodes, the branch outer diameters, wall thicknesses, material numbers, flexibility factors, stress intensification factors, internal fluid densities (DFL), exterior insulation densities (DIN) and thicknesses (TKIN), corrosion thickness allowance (TKCORR), and the isotropic material properties. The real constant material number (MAT), if supplied, overrides the element material property number applied with the MAT command, and defaults to the element material property number. The element degenerates to two branches if three nodes are input, and to one pipe element if only two nodes are input. The real constants (except DFL, DIN, and TKIN) for the other branches default to those of the first branch if not input. Properties not input default as described in Section 2.4.

The bending stiffness of this element is similar to that of BEAM4 except that it is modified by the flexibility factor. Each branch has its own element coordinate system, with its origin at the first node of the branch and the element X-axis along the branch axis. The orientation of the branch Y-axis is automatically calculated to be parallel to the global X-Y plane (see Figure 4.17-1). For the case where the branch is parallel to the global Z axis (or within a 0.01 percent slope of it), the branch Y-axis is oriented parallel to the global Y axis. Input and output locations around the pipe circumference identified as being at 0° are located along the branch Y-axis, and similarly 90° is along the branch Z-axis. The flexibility factor (FLEX) is divided into the cross-sectional moment of inertia to produce a modified moment of inertia for the stiffness calculation. FLEX defaults to 1.0 but may be input as any positive value. The internal fluid and external insulation constants are used only to determine the added mass effects for these components.

Element loads are described in Section 2.7. Pressures may be input as surface loads on the element faces as shown by the circled numbers on Figure 4.17-1. Internal pressure (PINT) and external pressure (POUT) are input as positive values. 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. See Section 14.16.7 of the ANSYS Theory Reference for details.

Temperatures may be input as element body loads at the nodes. Outer and inner wall temperatures may be specified for each branch. Temperatures are assumed to be uniform along each branch. The first temperature for branch 1 (TOUT1) defaults to TUNIF. If all temperatures after the first are unspecified, they default to the first. If both temperatures at branch 1 are input, and all temperatures at branches 2 and 3 are unspecified, they default to the corresponding branch 1 temperatures. For any other input pattern, unspecified temperatures default to TUNIF.

Use TREF and BETAD to supply global values for reference temperature and damping, respectively. Alternatively, use the MAT command to specify element-dependent values for reference temperature (MP,REFT) or damping (MP,DAMP); branch material numbers are ignored for this purpose.

The KEYOPT(2) options for stress intensification factors are discussed in Section 4.16.1.

A summary of the element input is given in Table 4.17-1. A general description of element input is given in Section 2.1.

Table 4.17-1 PIPE17 Input Summary

Element Name

PIPE17

Nodes

I, J, K, L for three branches (I-J, J-K, J-L), or
I, J, K for two branches (I-J, J-K), or
I, J for one branch (I-J)

Degrees of Freedom

UX, UY, UZ, ROTX, ROTY, ROTZ

Real Constants

OD1, TK1, MAT1, FLEX1, SIF1I, SIF1J,
OD2, TK2, MAT2, FLEX2, SIF2J, SIF2K,
OD3, TK3, MAT3, FLEX3, SIF3J, SIF3L,
DFL1, DIN1, TKIN1, DFL2, DIN2, TKIN2,
DFL3, DIN3, TKIN3, TKCORR

Material Properties

EX, ALPX, PRXY or NUXY, DENS, GXY, DAMP
REFT
Supply DAMP and REFT only once for the element (use MAT command to assign material property set). See the discussion in Section 4.17.1 for more details.

Surface Loads

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

Body Loads

Temperatures:
TOUT1, TIN1, TOUT2, TIN2, TOUT3, TIN3
(outer and inner for each branch)

Special Features

Stress stiffening, Large deflection, Birth and death.

KEYOPT(2)

0 - Stress intensity factors from SIF real constants
1 - Tee stress intensity factors at first node of each branch from tee joint calculation
2 - Tee stress intensity factors at second node of each branch from tee joint calculation
3 - Tee stress intensity factors at both nodes of each branch from tee joint calculation

KEYOPT(6)

0 - No printout of member forces or moments
2 - Print member forces and moments in the element coordinate system


4.17.2 Output Data

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

Several items are illustrated in Figure 4.17-2.

The direct stress includes the internal pressure (closed end) effect. The direct stress does not include the axial component of the transverse thermal stress. Also printed for each end of each branch 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. The effect of the corrosion allowance thickness is also included as described in Section 4.16.1. The principal stresses and the stress intensity include the shear force stress component. The output stresses and the stress intensification factors are calculated as shown in Section 4.16.1. Angles listed in the output are measured as shown () in Figure 4.17-2. A general description of solution output is given in Section 2.2. See the ANSYS Basic Analysis Procedures Guide for ways to view results.

Figure 4.17-2 PIPE17 Stress Output



The following notation is used in Table 4.17-2:

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 4.17-2 PIPE17 Element Output Definitions

Name

Definition

O

R

EL

Element number

Y Y
NODES

Nodes - I, J, K, L

Y Y
VOLU:

Volume

- Y
CENT: X, Y, Z

Center location XC, YC, ZC

- Y
TEMP

TOUT1,TIN1, TOUT2, TIN2, TOUT3, TIN3
(outer and inner for each branch)

Y Y
PRES

PINT, PX, PY, PZ, POUT

Y Y
MFOR(X, Y, Z)

Member forces at the ends of each branch
(in the branch coordinate system)

1 Y
MMOM(X, Y, Z)

Member moments at the ends of each branch
(in the branch coordinate system)

1 Y
SFACTI, SFACTJ

Stress intensification factors

2 2
STH

Stress due to maximum thermal gradient through the wall thickness

2 2
SPR2

Hoop pressure stress for code calculations

- 2
SMI, SMJ

Moment stress at nodes I and J for code calculations

- 2
SDIR

Direct (axial) stress

- 2
SBEND

Maximum bending stress at outer surface

- 2
ST

Shear stress at outer surface due to torsion

- 2
SSF

Shear stress due to shear force

- 2
S(1MX, 3MN,
INTMX, EQVMX)

Maximum principal stress, minimum principal stress, maximum stress intensity, maximum equivalent stress
(all at the outer surface)

2 2
S(1, 3, INT, EQV)

Maximum principal stress, minimum principal stress, stress intensity, equivalent stress

3 3
S(AXL, RAD, H, XH)

Axial, radial, hoop, and shear stresses

3 3
EPEL(AXL, RAD, H, XH)

Axial, radial, hoop, and shear strains

3 3
EPTH(AXL, RAD, H)

Axial, radial, and hoop thermal strain

3 3
1. Only if KEYOPT(6)=2

2. The item repeats for each branch

3. The item repeats at 0,45,90,135,180,225,270,315° at the ends of each branch (all at the outer surface)

The following tables list 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 Tables 4.17-3 through 4.17-3i:

Table 4.17-3 PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 1

Node I

Name

Item


E

Circumferential Location

0°

45°

90°

135°

180°

225°

270°

315°

SAXL

LS

- 1 5 9 13 17 21 25 29
SRAD

LS

- 2 6 10 14 18 22 26 30
SH

LS

- 3 7 11 15 19 23 27 31
SXH

LS

- 4 8 12 16 20 24 28 32
EPELAXL

LEPEL

- 1 5 9 13 17 21 25 29
EPELRAD

LEPEL

- 2 6 10 14 18 22 26 30
EPELH

LEPEL

- 3 7 11 15 19 23 27 31
EPELXH

LEPEL

- 4 8 12 16 20 24 28 32
EPTHAXL

LEPTH

- 1 5 9 13 17 21 25 29
EPTHRAD

LEPTH

- 2 6 10 14 18 22 26 30
EPTHH

LEPTH

- 3 7 11 15 19 23 27 31
S1

NMISC

- 1 6 11 16 21 26 31 36
S3

NMISC

- 3 8 13 18 23 28 33 38
SINT

NMISC

- 4 9 14 19 24 29 34 39
SEQV

NMISC

- 5 10 15 20 25 30 35 40
SBEND

NMISC

268 - - - - - - - -
SSF

NMISC

269 - - - - - - - -
MFORX

SMISC

1 - - - - - - - -
MFORY

SMISC

2 - - - - - - - -
MFORZ

SMISC

3 - - - - - - - -
MMOMX

SMISC

4 - - - - - - - -
MMOMY

SMISC

5 - - - - - - - -
MMOMZ

SMISC

6 - - - - - - - -
SDIR

SMISC

37 - - - - - - - -
ST

SMISC

38 - - - - - - - -
Table 4.17-3a PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 1

Node J

Name

Item


E

Circumferential Location

0°

45°

90°

135°

180°

225°

270°

315°

SAXL

LS

- 33 37 41 45 49 53 57 61
SRAD

LS

- 34 38 42 46 50 54 58 62
SH

LS

- 35 39 43 47 51 55 59 63
SXH

LS

- 36 40 44 48 52 56 60 64
EPELAXL

LEPEL

- 33 37 41 45 49 53 57 61
EPELRAD

LEPEL

- 34 38 42 46 50 54 58 62
EPELH

LEPEL

- 35 39 43 47 51 55 59 63
EPELXH

LEPEL

- 36 40 44 48 52 56 60 64
EPTHAXL

LEPTH

- 33 37 41 45 49 53 57 61
EPTHRAD

LEPTH

- 34 38 42 46 50 54 58 62
EPTHH

LEPTH

- 35 39 43 47 51 55 59 63
S1

NMISC

- 41 46 51 56 61 66 71 76
S3

NMISC

- 43 48 53 58 63 68 73 78
SINT

NMISC

- 44 49 54 59 64 69 74 79
SEQV

NMISC

- 45 50 55 60 65 70 75 80
SBEND

NMISC

270 - - - - - - - -
SSF

NMISC

271 - - - - - - - -
MFORX

SMISC

7 - - - - - - - -
MFORY

SMISC

8 - - - - - - - -
MFORZ

SMISC

9 - - - - - - - -
MMOMX

SMISC

10 - - - - - - - -
MMOMY

SMISC

11 - - - - - - - -
MMOMZ

SMISC

12 - - - - - - - -
SDIR

SMISC

39 - - - - - - - -
ST

SMISC

40 - - - - - - - -
Table 4.17-3b PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 1

Name

Item


E

Circumferential Location

0°

90°

180°

270°

SFACTI

NMISC

241 - - - -
SFACTJ

NMISC

242 - - - -
SPR2

NMISC

243 - - - -
SMI

NMISC

244 - - - -
SMJ

NMISC

245 - - - -
S1MX

NMISC

256 - - - -
S3MN

NMISC

257 - - - -
SINTMX

NMISC

258 - - - -
SEQVMX

NMISC

259 - - - -
STH

SMISC

41 - - - -
TOUT

LBFE

- 4 1 2 3
TIN

LBFE

- 8 5 6 7
Table 4.17-3c PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 2

Node J

Name

Item


E

Circumferential Location

0°

45°

90°

135°

180°

225°

270°

315°

SAXL

LS

- 65 69 73 77 81 85 89 93
SRAD

LS

- 66 70 74 78 82 86 90 94
SH

LS

- 67 71 75 79 83 87 91 95
SXH

LS

- 68 72 76 80 84 88 92 96
EPELAXL

LEPEL

- 65 69 73 77 81 85 89 93
EPELRAD

LEPEL

- 66 70 74 78 82 86 90 94
EPELH

LEPEL

- 67 71 75 79 83 87 91 95
EPELXH

LEPEL

- 68 72 76 80 84 88 92 96
EPTHAXL

LEPTH

- 65 69 73 77 81 85 89 93
EPTHRAD

LEPTH

- 66 70 74 78 82 86 90 94
EPTHH

LEPTH

- 67 71 75 79 83 87 91 95
S1

NMISC

- 81 86 91 96 101 106 111 116
S3

NMISC

- 83 88 93 98 103 108 113 118
SINT

NMISC

- 84 89 94 99 104 109 114 119
SEQV

NMISC

- 85 90 95 100 105 110 115 120
SBEND

NMISC

272 - - - - - - - -
SSF

NMISC

273 - - - - - - - -
MFORX

SMISC

13 - - - - - - - -
MFORY

SMISC

14 - - - - - - - -
MFORZ

SMISC

15 - - - - - - - -
MMOMX

SMISC

16 - - - - - - - -
MMOMY

SMISC

17 - - - - - - - -
MMOMZ

SMISC

18 - - - - - - - -
SDIR

SMISC

42 - - - - - - - -
ST

SMISC

43 - - - - - - - -
Table 4.17-3d PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 2

Node K

Name

Item


E

Circumferential Location

0°

45°

90°

135°

180°

225°

270°

315°

SAXL

LS

- 97 101 105 109 113 117 121 125
SRAD

LS

- 98 102 106 110 114 118 122 126
SH

LS

- 99 103 107 111 115 119 123 127
SXH

LS

- 100 104 108 112 116 120 124 128
EPELAXL

LEPEL

- 97 101 105 109 113 117 121 125
EPELRAD

LEPEL

- 98 102 106 110 114 118 122 126
EPELH

LEPEL

- 99 103 107 111 115 119 123 127
EPELXH

LEPEL

- 100 104 108 112 116 120 124 128
EPTHAXL

LEPTH

- 97 101 105 109 113 117 121 125
EPTHRAD

LEPTH

- 98 102 106 110 114 118 122 126
EPTHH

LEPTH

- 99 103 107 111 115 119 123 127
S1

NMISC

- 121 126 131 136 141 146 151 156
S3

NMISC

- 123 128 133 138 143 148 153 158
SINT

NMISC

- 124 129 134 139 144 149 154 159
SEQV

NMISC

- 125 130 135 140 145 150 155 160
SBEND

NMISC

274 - - - - - - - -
SSF

NMISC

275 - - - - - - - -
MFORX

SMISC

19 - - - - - - - -
MFORY

SMISC

20 - - - - - - - -
MFORZ

SMISC

21 - - - - - - - -
MMOMX

SMISC

22 - - - - - - - -
MMOMY

SMISC

23 - - - - - - - -
MMOMZ

SMISC

24 - - - - - - - -
SDIR

SMISC

44 - - - - - - - -
ST

SMISC

45 - - - - - - - -
Table 4.17-3e PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 2

Name

Item


E

Circumferential Location

0°

90°

180°

270°

SFACTI

NMISC

246 - - - -
SFACTJ

NMISC

247 - - - -
SPR2

NMISC

248 - - - -
SMI

NMISC

249 - - - -
SMJ

NMISC

250 - - - -
S1MX

NMISC

260 - - - -
S3MN

NMISC

261 - - - -
SINTMX

NMISC

262 - - - -
SEQVMX

NMISC

263 - - - -
STH

SMISC

46 - - - -
TOUT

LBFE

- 12 9 10 11
TIN

LBFE

- 16 13 14 15
Table 4.17-3f PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 3

Node J

Name

Item


E

Circumferential Location

0°

45°

90°

135°

180°

225°

270°

315°

SAXL

LS

- 129 133 137 141 145 149 153 157
SRAD

LS

- 130 134 138 142 146 150 154 158
SH

LS

- 131 135 139 143 147 151 155 159
SXH

LS

- 132 136 140 144 148 152 156 160
EPELAXL

LEPEL

- 129 133 137 141 145 149 153 157
EPELRAD

LEPEL

- 130 134 138 142 146 150 154 158
EPELH

LEPEL

- 131 135 139 143 147 151 155 159
EPELXH

LEPEL

- 132 136 140 144 148 152 156 160
EPTHAXL

LEPTH

- 129 133 137 141 145 149 153 157
EPTHRAD

LEPTH

- 130 134 138 142 146 150 154 158
EPTHH

LEPTH

- 131 135 139 143 147 151 155 159
S1

NMISC

- 161 166 171 176 181 186 191 196
S3

NMISC

- 163 168 173 178 183 188 193 198
SINT

NMISC

- 164 169 174 179 184 189 194 199
SEQV

NMISC

- 165 170 175 180 185 190 195 200
SBEND

NMISC

276 - - - - - - - -
SSF

NMISC

277 - - - - - - - -
MFORX

SMISC

25 - - - - - - - -
MFORY

SMISC

26 - - - - - - - -
MFORZ

SMISC

27 - - - - - - - -
MMOMX

SMISC

28 - - - - - - - -
MMOMY

SMISC

29 - - - - - - - -
MMOMZ

SMISC

30 - - - - - - - -
SDIR

SMISC

47 - - - - - - - -
ST

SMISC

48 - - - - - - - -
Table 4.17-3g PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 3

Node L

Name

Item


E

Circumferential Location

0°

45°

90°

135°

180°

225°

270°

315°

SAXL

LS

- 161 165 169 173 177 181 185 189
SRAD

LS

- 162 166 170 174 178 182 186 190
SH

LS

- 163 167 171 175 179 183 187 191
SXH

LS

- 164 168 172 176 180 184 188 192
EPELAXL

LEPEL

- 161 165 169 173 177 181 185 189
EPELRAD

LEPEL

- 162 166 170 174 178 182 186 190
EPELH

LEPEL

- 163 167 171 175 179 183 187 191
EPELXH

LEPEL

- 164 168 172 176 180 184 188 192
EPTHAXL

LEPTH

- 161 165 169 173 177 181 185 189
EPTHRAD

LEPTH

- 162 166 170 174 178 182 186 190
EPTHH

LEPTH

- 163 167 171 175 179 183 187 191
S1

NMISC

- 201 206 211 216 221 226 231 236
S3

NMISC

- 203 208 213 218 223 228 233 238
SINT

NMISC

- 204 209 214 219 224 229 234 239
SEQV

NMISC

- 205 210 215 220 225 230 235 240
SBEND

NMISC

278 - - - - - - - -
SSF

NMISC

279 - - - - - - - -
MFORX

SMISC

31 - - - - - - - -
MFORY

SMISC

32 - - - - - - - -
MFORZ

SMISC

33 - - - - - - - -
MMOMX

SMISC

34 - - - - - - - -
MMOMY

SMISC

35 - - - - - - - -
MMOMZ

SMISC

36 - - - - - - - -
SDIR

SMISC

49 - - - - - - - -
ST

SMISC

50 - - - - - - - -
Table 4.17-3h PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

BRANCH 3

Name

Item


E

Circumferential Location

0°

90°

180°

270°

SFACTI

NMISC

251 - - - -
SFACTJ

NMISC

252 - - - -
SPR2

NMISC

253 - - - -
SMI

NMISC

254 - - - -
SMJ

NMISC

255 - - - -
S1MX

NMISC

264 - - - -
S3MN

NMISC

265 - - - -
SINTMX

NMISC

266 - - - -
SEQVMX

NMISC

267 - - - -
STH

SMISC

51 - - - -
TOUT

LBFE

- 20 17 18 19
TIN

LBFE

- 24 21 22 23
Table 4.17-3i PIPE17 Item and Sequence Numbers for the ETABLE and ESOL Commands

Name

Item

E

PINT

SMISC

52
PX

SMISC

53
PY

SMISC

54
PZ

SMISC

55
POUT

SMISC

56

4.17.3 Assumptions and Restrictions

No branch can have a zero length or wall thickness (although branches may be deleted). In addition, the O.D. must not be less than or equal to zero, the I.D. must not be less than zero, and the corrosion thickness allowance must be less than the wall thickness. The element may be used for both thin and thick-walled situations; however, some of the stress calculations are based on thin-wall theory. The branches are assumed to have "closed ends" so that the axial pressure effect is included. There is no restriction on the angles of intersection of the branches. Shear deflection capability is also included in the element formulation.

4.17.4 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/LinearPlus