D13.E.5 Member Selection and Code Check
Both code checking and member selection options are available in SP 16.13330.2017.
Output of selection and check results are given in suppressed, extended and advanced forms. Form of output results depends on value of parameter TRACK.
Results are presented in tables. Three versions of output results are possible: suppressed – results according the critical strength condition (TRACK=0), extended - results according to all check conditions (TRACK=1) and advanced – complete information on results of member design (TRACK=2).
In tables of results common data for all TRACKs are indicated:
- (TRACK=2)
In tables of results common data for all TRACKs are indicated:
- number of member;
- type and number of cross-section;
- result obtained (ACCEPTED – requirements are met, FAILURE – are not met);
- abbreviated name of normative document (code, standard) (SNiP);
- number of check clause;
- safety of strength (ratio between design and normative values);
- number of the most unfavorable loading;
- value of longitudinal force acting in the member with subscript indicating its direction ("C" – compression, "T" – tension);
- bending moments in relation to local member axes Z and Y;
- distance to section, in which the most unfavorable combination of forces acts.
Refer to D1.B.1.3 Code Checking for general information on Code Checking. Refer to TR.49 Code Checking Specification for details the specification of the Code Checking command.
Refer to D1.B.1.4 Member Selection for general information on Member Selection. Refer to TR.49.1 Member Selection Specification for details the specification of the Member Selection command.
Note: The output for the Russian code uses the axes system from STAAD.Pro, except where details of the equations from the code are printed, in which case the axes system is as defined in the code.
D13.E.5.1 Example of TRACK 0 output
In suppressed form (TRACK 0) results are presented according to the critical check for given member with indication of SP 16 clause number, according to which strength safety of the member is minimum.
STAAD.PRO CODE CHECKING - (SP 16.13330.2017) V1.0
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ALL UNITS ARE - KN METRE
========================================================================
MEMBER CROSS RESULT/ CRITICAL COND/ RATIO/ LOADING/
SECTION NO. N Mx My LOCATION
========================================================================
* 384 GENERAL STABILITY CAN NOT BE CHECKED
FACTOR "ALPHA" < 0,1
(look at appendix G, table G.1) * Element is too short for checking the stability *
384 I SH100-4 PASS SP cl.9.1.1 0.23 3981
1.186E+00 C 9.442E+02 5.044E+00 1.000E+00
* 384 GENERAL STABILITY CAN NOT BE CHECKED
FACTOR "ALPHA" < 0,1
(look at appendix G, table G.1) * Element is too short for checking the stability *
384 I SH100-4 PASS DISPL 0.01 3981
1.186E+00 C 9.442E+02 5.044E+00 5.833E-01
1820 I SH3-50 PASS SP cl.9.1.1 0.41 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS DISPL 0.31 3655
1.627E+02 C 1.435E+00 7.986E+01 1.667E+00
1820 I SH3-50 PASS SP cl.10.4.1C 0.33 3655
1.627E+02 C 1.435E+00 -7.986E+01 0.000E+00
D13.E.5.2 Example of TRACK 1 output
In extended form (TRACK 1) results are presented on the basis of all required by SP 16 checks for given stress state.
STAAD.PRO CODE CHECKING - (SP 16.13330.2017) V1.0
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ALL UNITS ARE - KN METRE
========================================================================
MEMBER CROSS RESULT/ CRITICAL COND/ RATIO/ LOADING/
SECTION NO. N Mx My LOCATION
========================================================================
* 384 GENERAL STABILITY CAN NOT BE CHECKED
FACTOR "ALPHA" < 0,1
(look at appendix G, table G.1) * Element is too short for checking the stability *
384 I SH100-4 PASS SP cl.9.1.1 0.23 3981
1.186E+00 C 9.442E+02 5.044E+00 1.000E+00
384 I SH100-4 PASS SP cl.8.2.3 0.21 3981
1.186E+00 C 9.442E+02 5.044E+00 1.000E+00
* 384 GENERAL STABILITY CAN NOT BE CHECKED
FACTOR "ALPHA" < 0,1
(look at appendix G, table G.1) * Element is too short for checking the stability *
384 I SH100-4 PASS DISPL 0.01 3981
1.186E+00 C 9.442E+02 5.044E+00 5.833E-01
1820 I SH3-50 PASS SP cl.9.1.1 0.41 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.9.2.2 0.03 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.9.2.4 0.03 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.9.2.9 0.03 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.8.2.3 0.34 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.8.4.1 0.39 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS DISPL 0.31 3655
1.627E+02 C 1.435E+00 7.986E+01 1.667E+00
1820 I SH3-50 PASS SP cl.10.4.1C 0.33 3655
1.627E+02 C 1.435E+00 -7.986E+01 0.000E+00
D13.E.5.3 Example of a TRACK 2 output
In advanced form (TRACK=2) in addition to tabled results supplementary information is presented.
- Material characteristics:
- Steel;
- Design resistance;
- Elasticity modulus;
- Section characteristics:
- Length of member;
- Section area;
- Net area;
- Inertia moment (second moment of area) (I);
- Section modulus (W);
- First moment of area (S);
- Radius of gyration;
- Effective length;
- Slenderness;
- Results are presented in two columns, Z and Y respectively.
- Design forces:
- Longitudinal force;
- Moments;
- Shear force.
Signs "+" and "-" indicate direction of acting longitudinal force, bending moments and shear forces in accordance with sign rules assumed in program STAAD.Pro.
Check results in advanced form are presented with values of intermediate parameters by formulas in analytical and numerical expression with indication of SP code clause.
STAAD.PRO CODE CHECKING - (SP 16.13330.2017) V1.0
********************************************
ALL UNITS ARE - KN METRE
========================================================================
MEMBER CROSS RESULT/ CRITICAL COND/ RATIO/ LOADING/
SECTION NO. N Mx My LOCATION
========================================================================
* 384 GENERAL STABILITY CAN NOT BE CHECKED
FACTOR "ALPHA" < 0,1
(look at appendix G, table G.1) * Element is too short for checking the stability *
384 I SH100-4 PASS SP cl.9.1.1 0.23 3981
1.186E+00 C 9.442E+02 5.044E+00 1.000E+00
384 I SH100-4 PASS SP cl.8.2.3 0.21 3981
1.186E+00 C 9.442E+02 5.044E+00 1.000E+00
* 384 GENERAL STABILITY CAN NOT BE CHECKED
FACTOR "ALPHA" < 0,1
(look at appendix G, table G.1) * Element is too short for checking the stability *
384 I SH100-4 PASS DISPL 0.01 3981
1.186E+00 C 9.442E+02 5.044E+00 5.833E-01
MATERIAL DATA
Steel = C345B SP16.13330
Modulus of elasticity = 206.E+06 kPa
Design Strength (Ry) = 335.E+03 kPa
SECTION PROPERTIES (units - m, m^2, m^3, m^4)
Member Length = 1.00E+00
Gross Area = 4.01E-02
Net Area = 4.01E-02
x-axis y-axis
Moment of inertia (I) : 655.E-05 178.E-06
Section modulus (W) : 129.E-04 111.E-05
First moment of area (S) : 729.E-05 877.E-06
Radius of gyration (i) : 405.E-03 667.E-04
Effective Length : 1.00E+00 1.00E+00
Slenderness : 247.E-02 150.E-01
DESIGN DATA (units -kN,m) SP16.13330.2017
Axial force : 118.6E-02
x-axis y-axis
Moments : 944.2E+00 504.4E-02
Shear force : 410.6E-02 946.7E+00
Bi-moment : 0.000E+00 Value of Bi-moment not being entered!!!
CRITICAL CONDITIONS FOR EACH CLAUSE CHECK
F.(106) (N/A+Mx*y/Ix+My*x/Iy+B*w/Iw)/(Ry*GammaC)=
( 118.6E-02/ 4.0E-02+ 944.2E+00* 5.07E-01/ 6.55E-03+ 504.4E-02* 1.60E-01/
1.78E-04+ 0.000E+00* 2.50E-01/ 4.27E-05)/( 335.0E+03* 1.00E+00)
= 2.31E-01=<1
m_x =24.6E+02>20. m_y =15.3E+01>20.
F.(51) Mx/(Cx*beta*Wxn,min*Ry*GammaC)+My/(Cy*Wyn,min*Ry*GammaC)=
944.2E+00/( 1.11E+00* 9.99E-01* 1.29E-02* 335.0E+03* 1.00E+00)+
504.4E-02/( 1.15E+00* 1.11E-03* 335.0E+03* 1.00E+00)=
2.07E-01=<1
TAUX=Qx/Aw= 946.7E+00/ 197.5E-04= 479.E+02 <= 0,9*RS= 174.9E+03
TAUy=Qy/Af= 410.6E-02/ 208.0E-04= 197.E+00 <= 0,5*RS= 971.5E+02
LIMIT SPAN/DEFLECTION (DFF) = 250.00 (DEFLECTION LIMIT= 0.004 M)
SPAN/DEFLECTION = 177.2E+02 (DEFLECTION= 5.643E-05M)
LOAD= 3981 RATIO= 0.014 LOCATION= 0.583
STAAD.PRO CODE CHECKING - (SP 16.13330.2017) V1.0
********************************************
ALL UNITS ARE - KN METRE
========================================================================
MEMBER CROSS RESULT/ CRITICAL COND/ RATIO/ LOADING/
SECTION NO. N Mx My LOCATION
========================================================================
1820 I SH3-50 PASS SP cl.9.1.1 0.41 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.9.2.2 0.03 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.9.2.4 0.03 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.9.2.9 0.03 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.8.2.3 0.34 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS SP cl.8.4.1 0.39 3655
1.627E+02 C 1.435E+00 7.986E+01 0.000E+00
1820 I SH3-50 PASS DISPL 0.31 3655
1.627E+02 C 1.435E+00 7.986E+01 1.667E+00
1820 I SH3-50 PASS SP cl.10.4.1C 0.33 3655
1.627E+02 C 1.435E+00 -7.986E+01 0.000E+00
MATERIAL DATA
Steel = C345B SP16.13330
Modulus of elasticity = 206.E+06 kPa
Design Strength (Ry) = 335.E+03 kPa
SECTION PROPERTIES (units - m, m^2, m^3, m^4)
Member Length = 4.00E+00
Gross Area = 1.99E-02
Net Area = 1.99E-02
x-axis y-axis
Moment of inertia (I) : 842.E-06 925.E-07
Section modulus (W) : 340.E-05 617.E-06
First moment of area (S) : 192.E-05 462.E-06
Radius of gyration (i) : 206.E-03 681.E-04
Effective Length : 6.00E+00 4.00E+00
Slenderness : 292.E-01 587.E-01
DESIGN DATA (units -kN,m) SP16.13330.2017
Axial force : 162.7E+00
x-axis y-axis
Moments : 143.5E-02 798.6E-01
Shear force : 126.7E-01 400.1E-02
Bi-moment : 0.000E+00 Value of Bi-moment not being entered!!!
CRITICAL CONDITIONS FOR EACH CLAUSE CHECK
F.(106) (N/A+Mx*y/Ix+My*x/Iy+B*w/Iw)/(Ry*GammaC)=
( 162.7E+00/ 2.0E-02+ 143.5E-02* 2.48E-01/ 8.42E-04+ 798.6E-01* 1.50E-01/
9.25E-05+ 0.000E+00* 2.50E-01/ 5.19E-06)/( 335.0E+03* 1.00E+00)
= 4.12E-01=<1
P.9.2.2 m_ef=eta*mx= 0.00E+00* 5.17E-02= 0.00E+00
F.(109) N/(FIe*A*Ry*GammaC)= 162.7E+00/( 9.07E-01* 1.99E-02* 335.0E+03* 1.00E+00)
= 2.69E-02=<1
F.(112) C=beta/(1+alfa*mx)= 1.00E+00/(1+7.00E-01* 5.17E-02)= 9.65E-01
Cmax= 9.99E-01
F.(111) N/(c*FIy*A*Ry*GammaC)
= 0.16E+03/( 0.97E+00* 0.77E+00* 0.20E-01* 335.0E+03* 1.00E+00)
= 3.30E-02=<1
F.(117) FIexy=FIey*(0.6*C**(1/3)+0.4*C**(1/4))=
7.61E-01*(0.6*9.65E-01**(1/3)+0.4*9.65E-01**(1/4))= 7.53E-01
N/(FIexy*A*Ry*GammaC)= 162.7E+00/( 7.53E-01* 1.99E-02* 335.0E+03*1.00E+00)
=3.24E-02=<1
m_y =24.8E+00>20.
F.(51) Mx/(Cx*beta*Wxn,min*Ry*GammaC)+My/(Cy*Wyn,min*Ry*GammaC)=
143.5E-02/( 1.08E+00* 1.00E+00* 3.40E-03* 335.0E+03* 1.00E+00)+
798.6E-01/( 1.15E+00* 6.17E-04* 335.0E+03* 1.00E+00)=
3.37E-01=<1
TAUX=Qx/Aw= 400.1E-02/ 767.2E-05= 521.E+00 <= 0,9*RS= 174.9E+03
TAUy=Qy/Af= 126.7E-01/ 123.0E-04= 103.E+01 <= 0,5*RS= 971.5E+02
F.(70) Mx/(FIb*Wcx*Ry*GammaC)+My/(Wy*Ry*GammaC)+
B/(Ww*Ry*GammaC)=
1.44E+00/( 1.00E+00* 3.40E-03* 335.0E+03* 1.00E+00)+
7.99E+01/( 6.17E-04* 335.0E+03* 1.00E+00)+
0.00E+00/( 2.08E-05* 335.0E+03* 1.00E+00)= 3.88E-01=<1
LIMIT SPAN/DEFLECTION (DFF) = 250.00 (DEFLECTION LIMIT= 0.016 M)
SPAN/DEFLECTION = 809.8E+00 (DEFLECTION= 4.939E-03M)
LOAD= 3655 RATIO= 0.309 LOCATION= 1.667
ULTIM. SLENDERNESS >= Lambda_y 180.0E+00 >= 587.0E-01
Conventional notations assumed in presentation of results: "+", "-", "/", "*","**", "SQRT", their respective meanings (i.e., addition, subtraction, division, multiplication, raising to the second power (squared), and square root). Conventional notations of stresses, coefficients and characteristics of steel resistance comply with accepted in the SP standard. Only Greek letters are changed by their names (e.g., , γc-GAMAC; α-ALPHA; β-BETA, η-ETA, φ-PHI, etc.).