V. AIJ 2005 UPT Channel

Verify the bending capacity and compression capacity of a channel section beam.

Details

The member is a 5 m long simply-supported beam. The section used is a C380X100X10.5. The steel has a yield strength of 235 MPa, a modulus of elasticity of 205×(10)3 MPa, and a shear modulus of 79×(10)3 MPa.

The member is subject to the following loads:
  • a 10 kN·m concentrated moment at the left end
  • a -3 kN·m concentrated moment at the right end

Validation

Section Properties

Dimensions:

  • Depth, D = 380 mm
  • Width, B = 100 mm
  • Thickness of web, tw = 10.5 mm
  • Thickness of flange, tf = 16 mm

Height of web, d = D - 2tf = 348 mm

Area, Ax = 2B×tf + d×tw = 6,854 mm2

Distance from heel to centroid,

Moment of inertia about major axis,

Moment of inertia about minor axis,

Major axis section modulus,

Minor axis section modulus,

Torsional constant,

Warping constant,

Radius of gyration about major axis,

Radius of gyration about minor axis,

Section Classification

For webs of beams (Cl. 8.5):

Depth to thickness ratio is OK.

Allowable Compressive Stress

The slenderness ratio of compression members (Cl. 11.1):

Slenderness ratio dividing elastic and inelastic buckling (Cl no 5.5):

ν λ Ʌ

λ > Λ, so the allowable compressive stress is given by Cl. 5.4:

É…

Allowable Flexural Stress

Distance between braced points of the compression flange, lb = 5,000 mm.

The yield moment,

The modification factor for allowable flexural stress (Cl. 5.13):

The elastic lateral-torsional buckling moment (Cl 5.12):

The maximum slenderness ratio to achieve the plastic strength (Cl. 5.12):

The elastic slenderness limit:

Slenderness ratio of the flexural member,

Here, b < λb ≤ eλb , so:

Results

Table 1.
Result Type Reference STAAD.Pro Difference Comments
Allowable compressive stress (MPa) 33.35 33.34 negligible
Allowable flexural stress (MPa) 102.5 102.48 negligible

STAAD.Pro Input

The file C:\Users\Public\Public Documents\STAAD.Pro 2024\Samples \Verification Models\09 Steel Design\Japan\AIJ 2005 UPT Channel.STD is typically installed with the program.

STAAD SPACE
START JOB INFORMATION
ENGINEER DATE 22-Oct-18
END JOB INFORMATION
INPUT WIDTH 79
UNIT METER KN
JOINT COORDINATES
31 19 0 0; 32 24 0 0;
MEMBER INCIDENCES
16 31 32;
START USER TABLE
TABLE 1
UNIT METER KN
GENERAL
GE_H300X150X6.5X9
0.004678 0.3 0.0065 0.15 0.009 7.21e-05 5.08e-06 9.95e-08 0.000480667 -
6.77333e-05 0.00195 0.0018 0 0 1.07545e-07 0.256
*0.004678 0.3 0 0.15 0 7.21e-05 5.08e-06 9.95e-08 0.000480667 6.77333e-05 -
*0.00195 0.0018 0 0 1.07545e-07 0.256
TABLE 2
UNIT METER KN
WIDE FLANGE
WF_H300X150X6.5X9
0.004678 0.3 0.0065 0.15 0.009 7.21e-05 5.08e-06 9.95e-08 0.00195 0.0018
WF2_H300X150X6.5X9
0.004678 0.3 0.0065 0.15 0.009 7.21e-05 5.08e-06 9.95e-08 0.00195 -
0.0018 0.15 0.009
WF_H300X100-200X7X9-12
0.005253 0.3 0.007 0.1 0.009 7.29942e-05 8.75797e-06 1.71399e-07 0.0021 -
0.0022 0.2 0.012
TABLE 3
UNIT METER KN
ISECTION
IS_I300X150X8
0.3 0.008 0.3 0.15 0.013 0.15 0.013 0.0024 0.0026 2.69e-07
TABLE 4
UNIT METER KN
CHANNEL
CH_C380X100X10.5
0.006854 0.38 0.0105 0.1 0.016 0.000142897 6.11657e-06 4.07351e-07 -
0.0261429 0.00399 0.00213333
TABLE 5
UNIT METER KN
ANGLE
AG_L175X175X15
0.175 0.175 0.015 0.0342 0.00175 0.00175
TABLE 6
UNIT METER KN
TUBE
TB_TUB1501506
0.003363 0.15 0.15 0.006 1.15e-05 1.15e-05 1.79e-05 0.0018 0.0018
TB_RHS200X100X9
0.004867 0.2 0.1 0.009 2.35e-05 7.82e-06 1.93e-05 0.0036 0.0018
TABLE 7
UNIT METER KN
PIPE
PP_PIP165.2X7.1
0.1652 0.151 0.001763 0.001763
TABLE 8
UNIT METER KN
DOUBLE ANGLE
DA_L100X100X13LD
0.1 0.1 0.013 0 4.48744e-06 8.79409e-06 2.73893e-07 0.0294 0.00173333 -
0.00173333 1.94
TABLE 9
UNIT METER KN
TEE
TE_CT100X200X8X12
0.003177 0.1 0.2 0.012 0.008 1.84e-06 8.01e-06 1.3e-07 0.0173 0.000533333 -
0.0016
END
DEFINE MATERIAL START
ISOTROPIC STEEL
E 2.05e+08
POISSON 0.3
DENSITY 76.8195
ALPHA 1.2e-05
DAMP 0.03
TYPE STEEL
STRENGTH RY 1.5 RT 1.2
END DEFINE MATERIAL
MEMBER PROPERTY JAPANESE
16 UPTABLE 4 CH_C380X100X10.5
CONSTANTS
MATERIAL STEEL ALL
SUPPORTS
31 PINNED
32 FIXED BUT FX MY MZ
LOAD 1 LOADTYPE None  TITLE LOAD CASE 1
JOINT LOAD
31 MZ 10
32 MZ -3
*148 FX 0.01 FY 0.01 MX 0.8
PERFORM ANALYSIS
PARAMETER 1
CODE JAPANESE 2005
TRACK 2 ALL
CHECK CODE ALL
PRINT MEMBER PROPERTIES ALL
FINISH

STAAD.Pro Output

                        STAAD.Pro CODE CHECKING - (AIJ-2005)   V2.1
                        ***********************
ALL UNITS ARE IN - METE  KN   (U.N.O.)
|-----------------------------------------------------------------------------|
|   Member No:      16        Profile  : CH_C380X100X10(UPT)                    |
|  Ratio:    0.130  (PASS)  Reference: Eq.5.8            Loadcase:       1    |
|-----------------------------------------------------------------------------|
|  Location:    0.000  Criteria:     Stress      Load Case:     1  (Permanent)|
|  Px:(C)        0.000       Vy:         1.400          Vz:       0.000       |
|  Tx:           0.000       My:         0.000          Mz:      10.000       |
|-----------------------------------------------------------------------------|
| SECTION PROPERTIES AT DISTANCE:    0.000 MM              (UNIT: MM)         |
|  Ax:     6.85400E+03       Az: 2.13333E+03            Ay: 3.99000E+03       |
|  Iz:     1.42897E+08       Iy: 6.11657E+06             J: 4.07351E+05       |
|  Zz:     7.52090E+05       Zy: 8.28163E+04            Zx: 2.54594E+04       |
|  iZ:     1.44391E+02       iY: 2.98732E+01            Iw: 1.44256E+11       |
|-----------------------------------------------------------------------------|
| MATERIAL PROPERTIES   (Unit: N/mm2)                                         |
|  Fy:         235.000      E :   205000.000          G :     79000.000       |
|-----------------------------------------------------------------------------|
| DESIGN PROPERTIES                                                           |
|  Member Length:     5.000      Lz:     5.000 Ly:     5.000  UNL:      5.000 |
| DESIGN PARAMETERS                                                           |
|  Kz:   1.000     Ky:   1.000   NSF:  1.000   Cb:   0.000    pλb:  0.000     |
|-----------------------------------------------------------------------------|
| CRITICAL SLENDERNESS (Tension)                                              |
|  Actual :    167.374      Allowable :    400.000      Ratio :  0.418        |
|-----------------------------------------------------------------------------|
| Section Classification Results :    Width to Thickness Ratios               |
|-----------------------------------------------------------------------------|
|            Compression              |             Bending                   |
|-----------------------------------------------------------------------------|
|  LC#   |    Actual   |   Allowable  |   LC#   |    Actual   |   Allowable   |
|-----------------------------------------------------------------------------|
|   -    |      -      |       -      |      1  |    33.1429  |     70.8850   |
|-----------------------------------------------------------------------------|
| CHECKS                              |Env|     Stresses    |                 |
|              | Loc. | Demand |  L/C |Typ| Actual | Allow  |Ratio |   Ref.   |
|              |(MET) |(KN-MET)|      |   |(N/mm2) |(N/mm2) |      |          |
|--------------|------|--------|------|---|--------|--------|------|----------|
| Tension      |  -   |   -    |  -   | - |   -    |  156.67|  -   | Eq.5.1   | 
| Compression  |  -   |   -    |  -   | - |   -    |   33.34|  -   | Eq.5.4   |  
| Bending Z (T)| 0.000|   10.00|     1| P |   13.30|  156.67| 0.085| Eq.5.1   | 
| Bending Z (C)| 0.000|   10.00|     1| P |   13.30|  102.48| 0.130| Eq.5.8   |  
| Bending Y (T)|  -   |   -    |  -   | - |   -    |  156.67|  -   | Eq.5.1   | 
| Bending Y (C)|  -   |   -    |  -   | - |   -    |  156.67|  -   | Eq.5.1   | 
| Shear Z      |  -   |   -    |  -   | - |   -    |   90.45|  -   | Eq.5.2   | 
| Shear Y      | 0.000|    1.40|     1| P |    0.35|   90.45| 0.004| Eq.5.2   | 
| Comp+ Bend C | 0.000|   -    |     1| P |   -    |    -   | 0.130| Eq.6.1   | 
| Comp+ Bend T | 0.000|   -    |     1| P |   -    |    -   | 0.085| Eq.6.2   | 
| Ten + Bend T | 0.000|   -    |     1| P |   -    |    -   | 0.085| Eq.6.3   | 
| Ten + Bend C | 0.000|   -    |     1| P |   -    |    -   | 0.130| Eq.6.4   | 
| Von-Mises    | 0.000|   -    |     1| P |   13.31|  156.67| 0.085| Eq.5.24  | 
|                                                                             |
| INTERMEDIATE RESULTS (Bending)                                              |
|  Me: 2.1541E+02 KN-MET  My: 1.7674E+02 KN-MET   pλb:   0.510  C:  1.462     |
|                                                                             |
| INTERMEDIATE RESULTS (Von-Mises)                                            |
|  Sigmax:    13.296 N/mm2   Tou:     0.351 N/mm2  fm:    13.310 N/mm2        |
|-----------------------------------------------------------------------------|