V. CSA 086 2001 - Beam in Bending
Reference
Example 1, page 58, Canadian Wood Design Manual, 2001
Given
Length =6,000mm, Beam Spacing = 3,000mm, Standard load condition, Dry service condition, Untreated
Comparison
Criteria | Reference | STAAD.Pro | Difference |
---|---|---|---|
Design Strength in Bending (kN·m) | 79.8 | 79.732 | none |
Design Strength in Shear (kN) | 46.1 | 46.170 | none |
STAAD Input
The file C:\Users\Public\Public Documents\STAAD.Pro 2024\Samples \Verification Models\11 Timber Design\Canada\CSA 086 2001 - Beam in Bending.STD is typically installed with the program.
STAAD PLANE
START JOB INFORMATION
ENGINEER DATE 08-JUN-05
END JOB INFORMATION
UNIT METER KN
JOINT COORDINATES
1 0 0 0; 2 6 0 0; 3 3 0 0;
MEMBER INCIDENCES
1 1 3; 2 3 2;
UNIT FEET POUND
DEFINE MATERIAL START
ISOTROPIC DFL_NO1_10X16_BM
E 1.728e+06
POISSON 0.15
DENSITY 25
ALPHA 5.5e-06
END DEFINE MATERIAL
UNIT METER KN
CONSTANTS
MATERIAL DFL_NO1_10X16_BM ALL
UNIT FEET POUND
MEMBER PROPERTY TIMBER CANADIAN
1 2 TABLE ST DFL_NO1_10X16_BM
SUPPORTS
1 2 FIXED
UNIT METER KN
LOAD 1 DEAD+LIVE LOAD
MEMBER LOAD
1 2 UNI GY -16.4
PERFORM ANALYSIS
PARAMETER 1
CODE TIMBER CANADIAN
KD 1 ALL
K_T 1 ALL
KSB 1 ALL
KZB 0.9 ALL
KZV 0.9 ALL
K_ZC 1.05 ALL
CHECK CODE ALL
FINISH
STAAD Output
STAAD.Pro CODE CHECKING - (S086) v1.0
***********************
ALL UNITS ARE - KN METE (UNLESS OTHERWISE Noted)
MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/
FX MY MZ LOCATION
=======================================================================
1 ST DFL_NO1_10X16_BM
FAIL CL.5.5.5/6.5.6 1.066 1
0.00 T 0.00 49.20 0.0000
|--------------------------------------------------------------------------|
| LEZ = 3000.000 LEY = 3000.000 LUZ = 3000.000 LUY = 3000.000mm |
| |
| KD = 1.000 KH = 1.000 KT = 1.000 KSB = 1.000 KSV = 1.000 |
| KSC = 1.000 K_SCP = 1.000 KSE = 1.000 KST = 1.000 KZB = 0.900 |
| KZV = 0.900 KZT = 1.000 KZCP = 1.000 K_ZC = 1.050 CHIX = 1.000 |
| CV = 1.000 KN = 1.000 |
| |
| ACTUAL LOADS : (KN-m) |
| Pu = 0.000 |
| Tu = 0.000 |
| Muy = 0.000 |
| Muz = 49.200 |
| V = 49.200 |
| SLENDERNESS_Y = 4.511 |
| SLENDERNESS_Z = 2.158 |
| ALLOWABLE CAPACITIES OF THE SECTION: (KN-m) |
| PY = 0.000 |
| PZ = 0.000 |
| T = 0.000 |
| MY = 79.800 |
| MZ = 79.732 |
| V = 46.170 |
| SLENDERNESS = 50.000 |
|--------------------------------------------------------------------------|
STAAD PLANE -- PAGE NO. 4
ALL UNITS ARE - KN METE (UNLESS OTHERWISE Noted)
MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/
FX MY MZ LOCATION
=======================================================================
2 ST DFL_NO1_10X16_BM
FAIL CL.5.5.5/6.5.6 1.066 1
0.00 T 0.00 49.20 3.0000
|--------------------------------------------------------------------------|
| LEZ = 3000.000 LEY = 3000.000 LUZ = 3000.000 LUY = 3000.000mm |
| |
| KD = 1.000 KH = 1.000 KT = 1.000 KSB = 1.000 KSV = 1.000 |
| KSC = 1.000 K_SCP = 1.000 KSE = 1.000 KST = 1.000 KZB = 0.900 |
| KZV = 0.900 KZT = 1.000 KZCP = 1.000 K_ZC = 1.050 CHIX = 1.000 |
| CV = 1.000 KN = 1.000 |
| |
| ACTUAL LOADS : (KN-m) |
| Pu = 0.000 |
| Tu = 0.000 |
| Muy = 0.000 |
| Muz = 49.200 |
| V = -49.200 |
| SLENDERNESS_Y = 4.511 |
| SLENDERNESS_Z = 2.158 |
| ALLOWABLE CAPACITIES OF THE SECTION: (KN-m) |
| PY = 0.000 |
| PZ = 0.000 |
| T = 0.000 |
| MY = 79.800 |
| MZ = 79.732 |
| V = 46.170 |
| SLENDERNESS = 50.000 |
|--------------------------------------------------------------------------|