STAAD EDITORSTAAD TRUSSSTART JOB INFORMATIONENGINEER DATE 17-Mar-15END JOB INFORMATIONINPUT WIDTH 79UNIT METER KNJOINT COORDINATES1 0 0 0; 2 3.81001 0 0; 3 7.62002 0 0; 4 11.43 0 0; 5 15.24 0 0;6 1.905 1.905 0; 7 5.71501 1.905 0; 8 9.52502 1.905 0; 9 13.335 1.905 0;MEMBER INCIDENCES1 1 2; 2 2 3; 3 3 4; 4 4 5; 5 6 7; 6 7 8; 7 8 9; 8 1 6; 9 6 2; 10 2 7; 11 7 3;12 3 8; 13 8 4; 14 4 9; 15 9 5;DEFINE MATERIAL STARTISOTROPIC STEELE 1.99947e+008POISSON 0.3DENSITY 76.8191ALPHA 6.5e-006DAMP 0.03END DEFINE MATERIALMEMBER PROPERTY INDIAN1 TO 8 15 TABLE LD ISA100X100X109 TO 14 TABLE LD ISA80X80X12CONSTANTSMATERIAL STEEL ALLSUPPORTS1 PINNED5 FIXED BUT FX FZ MX MY MZLOAD 1 LOADTYPE None TITLE LOAD CASE 1JOINT LOAD2 4 FY -503 FY -75PERFORM ANALYSIS PRINT ALLPARAMETER 1CODE IS800 LSDBEAM 1 ALLDFF 325 ALLFYLD 415000 ALLRATIO 1 ALLCHECK CODE ALLPARAMETER 2CODE IS800 LSDSTEEL MEMBER TAKE OFF LIST 1 TO 15PARAMETER 3CODE IS800 LSDSELECT ALLPARAMETER 4CODE IS800 LSDSTEEL TAKE OFF LIST 1 TO 15FINISH

OUTPUT FILE

STAAD.Pro CODE CHECKING - (ILSD) ***********************

ALL UNITS ARE - KN METE (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION =======================================================================

1 LD ISA100X100X10 (INDIAN SECTIONS) PASS TENSION 0.061 1 87.50 T 0.00 0.00 0.00 2 LD ISA100X100X10 (INDIAN SECTIONS) PASS TENSION 0.148 1 212.50 T 0.00 0.00 0.00 3 LD ISA100X100X10 (INDIAN SECTIONS) PASS TENSION 0.148 1 212.50 T 0.00 0.00 0.00 4 LD ISA100X100X10 (INDIAN SECTIONS) PASS TENSION 0.061 1 87.50 T 0.00 0.00 0.00 5 LD ISA100X100X10 (INDIAN SECTIONS) PASS COMPRESSION 0.518 1 175.00 C 0.00 0.00 0.00 6 LD ISA100X100X10 (INDIAN SECTIONS) PASS COMPRESSION 0.740 1 250.00 C 0.00 0.00 0.00 7 LD ISA100X100X10 (INDIAN SECTIONS) PASS COMPRESSION 0.518 1 175.00 C 0.00 0.00 0.00 8 LD ISA100X100X10 (INDIAN SECTIONS) PASS COMPRESSION 0.215 1 123.74 C 0.00 0.00 0.00 9 LD ISA80X80X12 (INDIAN SECTIONS) PASS TENSION 0.092 1 123.74 T 0.00 0.00 0.00 STAAD TRUSS -- PAGE NO. 6

ALL UNITS ARE - KN METE (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION =======================================================================

10 LD ISA80X80X12 (INDIAN SECTIONS) PASS COMPRESSION 0.142 1 53.03 C 0.00 0.00 0.00 11 LD ISA80X80X12 (INDIAN SECTIONS) PASS TENSION 0.039 1 53.03 T 0.00 0.00 0.00 12 LD ISA80X80X12 (INDIAN SECTIONS) PASS TENSION 0.039 1 53.03 T 0.00 0.00 0.00 13 LD ISA80X80X12 (INDIAN SECTIONS) PASS COMPRESSION 0.142 1 53.03 C 0.00 0.00 0.00 14 LD ISA80X80X12 (INDIAN SECTIONS) PASS TENSION 0.092 1 123.74 T 0.00 0.00 0.00 15 LD ISA100X100X10 (INDIAN SECTIONS) PASS COMPRESSION 0.215 1 123.74 C 0.00 0.00 0.00 ************** END OF TABULATED RESULT OF DESIGN **************

41. PARAMETER 2 42. CODE IS800 LSD 43. STEEL MEMBER TAKE OFF LIST 1 TO 15 STAAD TRUSS -- PAGE NO. 7

STEEL TAKE-OFF -------------- PROFILE LENGTH(METE) WEIGHT(KN )

LD ISA100X100X10 32.06 9.373 LD ISA80X80X12 16.16 4.423 ---------------- TOTAL = 13.796

MEMBER PROFILE LENGTH WEIGHT (METE) (KN )

1 LD ISA100X100X10 3.81 1.114 2 LD ISA100X100X10 3.81 1.114 3 LD ISA100X100X10 3.81 1.114 4 LD ISA100X100X10 3.81 1.114 5 LD ISA100X100X10 3.81 1.114 6 LD ISA100X100X10 3.81 1.114 7 LD ISA100X100X10 3.81 1.114 8 LD ISA100X100X10 2.69 0.788 9 LD ISA80X80X12 2.69 0.737 10 LD ISA80X80X12 2.69 0.737 11 LD ISA80X80X12 2.69 0.737 12 LD ISA80X80X12 2.69 0.737 13 LD ISA80X80X12 2.69 0.737 14 LD ISA80X80X12 2.69 0.737 15 LD ISA100X100X10 2.69 0.788 ---------------- TOTAL = 13.796 ************ END OF DATA FROM INTERNAL STORAGE ************ 44. PARAMETER 3 45. CODE IS800 LSD 46. SELECT ALL STAAD TRUSS -- PAGE NO. 8

STAAD.Pro MEMBER SELECTION - (ILSD) **************************

ALL UNITS ARE - KN METE (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION =======================================================================

1 LD ISA45X45X3 (INDIAN SECTIONS) PASS TENSION 0.928 1 87.50 T 0.00 0.00 0.00 2 LD ISA45X30X6 (INDIAN SECTIONS) PASS TENSION 0.908 1 212.50 T 0.00 0.00 0.00 3 LD ISA45X30X6 (INDIAN SECTIONS) PASS TENSION 0.908 1 212.50 T 0.00 0.00 0.00 4 LD ISA45X45X3 (INDIAN SECTIONS) PASS TENSION 0.928 1 87.50 T 0.00 0.00 0.00 5 LD ISA100X100X6 (INDIAN SECTIONS) PASS COMPRESSION 0.820 1 175.00 C 0.00 0.00 0.00 6 LD ISA125X95X6 (INDIAN SECTIONS) PASS COMPRESSION 0.827 1 250.00 C 0.00 0.00 0.00 7 LD ISA100X100X6 (INDIAN SECTIONS) PASS COMPRESSION 0.820 1 175.00 C 0.00 0.00 0.00 8 LD ISA75X75X5 (INDIAN SECTIONS) PASS COMPRESSION 0.849 1 123.74 C 0.00 0.00 0.00 9 LD ISA40X40X4 (INDIAN SECTIONS) PASS TENSION 0.971 1 123.74 T 0.00 0.00 0.00 STAAD TRUSS -- PAGE NO. 9

ALL UNITS ARE - KN METE (UNLESS OTHERWISE NOTED) MEMBER TABLE RESULT/ CRITICAL COND/ RATIO/ LOADING/ FX MY MZ LOCATION =======================================================================

10 LD ISA65X45X5 (INDIAN SECTIONS) PASS COMPRESSION 0.857 1 53.03 C 0.00 0.00 0.00 11 LD ISA35X35X3 (INDIAN SECTIONS) PASS TENSION 0.951 1 53.03 T 0.00 0.00 0.00 12 LD ISA35X35X3 (INDIAN SECTIONS) PASS TENSION 0.951 1 53.03 T 0.00 0.00 0.00 13 LD ISA65X45X5 (INDIAN SECTIONS) PASS COMPRESSION 0.857 1 53.03 C 0.00 0.00 0.00 14 LD ISA40X40X4 (INDIAN SECTIONS) PASS TENSION 0.971 1 123.74 T 0.00 0.00 0.00 15 LD ISA75X75X5 (INDIAN SECTIONS) PASS COMPRESSION 0.849 1 123.74 C 0.00 0.00 0.00 ************** END OF TABULATED RESULT OF DESIGN **************

47. PARAMETER 4 48. CODE IS800 LSD 49. STEEL TAKE OFF LIST 1 TO 15 STAAD TRUSS -- PAGE NO. 10

STEEL TAKE-OFF -------------- PROFILE LENGTH(METE) WEIGHT(KN )

LD ISA45X45X3 7.62 0.309 LD ISA45X30X6 7.62 0.487 LD ISA100X100X6 7.62 1.366 LD ISA125X95X6 3.81 0.753 LD ISA75X75X5 5.39 0.602 LD ISA40X40X4 5.39 0.254 LD ISA65X45X5 5.39 0.435 LD ISA35X35X3 5.39 0.168 ---------------- TOTAL = 4.375 ************ END OF DATA FROM INTERNAL STORAGE ************ 50. FINISHDEFLECTION DIAGRAM

AXIAL FORCE DIAGRAM

STEEL DESIGN

BEAM NO:5

BEAM NO:10

BEAM NO:3

Design Of Member No. 15 As Per IS:800Input ParametersMember Section 2XISA100X100X10 - 0 mm long leg back-to-backCross Sectional Area Ax (m 2) 0.00rz (m ) 0.03ry (m ) 0.04Section Modulus About Major Axis - Tension Edge Stz (m 3) 0.00Section Modulus About Major Axis - Compression Edge Szz (m 3) 0.00Section Modulus About Minor Axis - Tension Edge Sty (m 3) 0.00Section Modulus About Minor Axis - Compression Edge Syy (m 3) 0.00Unsupported Length - Major Axis For Slenderness Check Lz (m ) 2.69Unsupported Length - Minor Axis For Slenderness Check Ly (m ) 2.69Effective Length For Allowable Bending Stress Calculation Unl (m ) 2.69Yield Stress fy (MPa) 415.00Allowable Ratio For Interaction Check 1.00Design ForcesCombined Axial Force & Bi-axial momentAxial Load Fx (kN ) 123.74Major Axis Moment Mz (kN m ) 0.00Minor Axis Moment My (kN m ) 0.00Critical Loadcase No. 1Critical Section (m ) 0.00Beam No. 8No Shear Force Developed Along Major AxisNo Shear Force Developed Along Minor AxisDetails Of CalculationSlenderness CheckingLez (m ) 2.69Ley (m ) 2.69Lez / rz87.60Ley / ry64.11Actual Slenderness Ratio 87.60Allowable Slenderness Ratio 180.00Status SAFECheck Against Axial Compression And Bi-Axial BendingActual Compressive Stress fc (MPa) =Fx / Ax32.51Calculation Of Allowable Compressive Stress :E (MPa) 200000.00L / r 87.60fcc (MPa) =p 2 E / l 2 257.25Allowable Compressive Stress fc_allowable (MPa) =0.6fccfy / [(fcc) 1.4+ (fy) 1.4] 114.88No Bending Moment Developed Along Major AxisNo Bending Moment Developed Along Minor AxisInteraction CheckingCmz0.85Cmy0.85Elastic Critical Stress For Bending About Major Axis fccz (MPa) =p 2 E / (L / rz)2257.18Elastic Critical Stress For Bending About Minor Axis fccy (MPa) =p 2 E / (L / ry)2480.19Interaction ratio =fc / fc_allowable + Cmzfcz / [(1 - fc / 0.60fccz)fcz_allowable] +Cmyfcy / [(1 - fc / 0.60fccy)fcy_allowable] 0.28Status SAFEDeflection Checking IgnoredDesign Of Member No. 22 As Per IS:800Input ParametersMember Section 2XISA100X100X10 - 0 mm long leg back-to-backCross Sectional Area Ax (m 2) 0.00Net section factor 1.00Net Effective Sectional Area Anet (m 2) 0.00rz (m ) 0.03ry (m ) 0.04Section Modulus About Major Axis - Tension Edge Stz (m 3) 0.00Section Modulus About Major Axis - Compression Edge Szz (m 3) 0.00Section Modulus About Minor Axis - Tension Edge Sty (m 3) 0.00Section Modulus About Minor Axis - Compression Edge Syy (m 3) 0.00Unsupported Length - Major Axis For Slenderness Check Lz (m ) 3.81Unsupported Length - Minor Axis For Slenderness Check Ly (m ) 3.81Effective Length For Allowable Bending Stress Calculation Unl (m ) 3.81Yield Stress fy (MPa) 415.00Allowable Ratio For Interaction Check 1.00Design ForcesCombined Axial Force & Bi-axial momentAxial Load Fx (kN ) -212.50Major Axis Moment Mz (kN m ) 0.00Minor Axis Moment My (kN m ) 0.00Critical Loadcase No. 1Critical Section (m ) 0.00Beam No. 2No Shear Force Developed Along Major AxisNo Shear Force Developed Along Minor AxisDetails Of CalculationSlenderness CheckingLez (m ) 3.81Ley (m ) 3.81Lez / rz123.88Ley / ry90.66Actual Slenderness Ratio 123.88Allowable Slenderness Ratio 400.00Status SAFECheck Against Axial Tension And Bi-Axial BendingActual Tensile Stress ft (MPa) =Fx / Anet 55.83Allowable Tensile Stress ft_allowable (MPa) =0.60fy 249.00Actual Bending Tensile Stress - Major Axis ftz (MPa) =Mz / Stz0.00Allowable Bending Tensile Stress - Major Axis ftz_allowable (MPa) =0.66fy273.90Actual Bending Tensile Stress - Minor Axis fty (MPa) =My / Sty0.00Allowable Bending Tensile Stress - Minor Axis fty_allowable (MPa) =0.66fy273.90Interaction CheckingInteraction ratio =ft / ft_allowable + ftz / ftz_allowable + fty / fty_allowable0.22Status SAFEDeflection Checking IgnoredDesign Of Member No. 28 As Per IS:800Input ParametersMember Section 2XISA80X80X12 - 0 mm long leg back-to-backCross Sectional Area Ax (m 2) 0.00rz (m ) 0.02ry (m ) 0.03Section Modulus About Major Axis - Tension Edge Stz (m 3) 0.00Section Modulus About Major Axis - Compression Edge Szz (m 3) 0.00Section Modulus About Minor Axis - Tension Edge Sty (m 3) 0.00Section Modulus About Minor Axis - Compression Edge Syy (m 3) 0.00Unsupported Length - Major Axis For Slenderness Check Lz (m ) 2.69Unsupported Length - Minor Axis For Slenderness Check Ly (m ) 2.69Effective Length For Allowable Bending Stress Calculation Unl (m ) 2.69Yield Stress fy (MPa) 415.00Allowable Ratio For Interaction Check 1.00Design ForcesCombined Axial Force & Bi-axial momentAxial Load Fx (kN ) 53.03Major Axis Moment Mz (kN m ) 0.00Minor Axis Moment My (kN m ) 0.00Critical Loadcase No. 1Critical Section (m ) 0.00Beam No. 13No Shear Force Developed Along Major AxisNo Shear Force Developed Along Minor AxisDetails Of CalculationSlenderness CheckingLez (m ) 2.69Ley (m ) 2.69Lez / rz111.93Ley / ry78.75Actual Slenderness Ratio 111.93Allowable Slenderness Ratio 180.00Status SAFECheck Against Axial Compression And Bi-Axial BendingActual Compressive Stress fc (MPa) =Fx / Ax14.89Calculation Of Allowable Compressive Stress :E (MPa) 200000.00L / r 111.93fcc (MPa) =p 2 E / l 2 157.54Allowable Compressive Stress fc_allowable (MPa) =0.6fccfy / [(fcc) 1.4+ (fy) 1.4] 80.24No Bending Moment Developed Along Major AxisNo Bending Moment Developed Along Minor AxisInteraction CheckingCmz0.85Cmy0.85Elastic Critical Stress For Bending About Major Axis fccz (MPa) =p 2 E / (L / rz)2157.50Elastic Critical Stress For Bending About Minor Axis fccy (MPa) =p 2 E / (L / ry)2318.19Interaction ratio =fc / fc_allowable + Cmzfcz / [(1 - fc / 0.60fccz)fcz_allowable] +Cmyfcy / [(1 - fc / 0.60fccy)fcy_allowable] 0.19Status SAFEDeflection Checking Ignored