Good Morning Bentley Support,
I have a query in the staad model (TEXT CODE) attached in the email.
STAAD PLANE START JOB INFORMATION ENGINEER DATE 24-Aug-17 END JOB INFORMATION INPUT WIDTH 79 UNIT METER KN JOINT COORDINATES 472 0 0 0; 2283 5.8 0 0; MEMBER INCIDENCES 5169 472 2283; DEFINE MATERIAL START ISOTROPIC CONCRETE E 2.17185e+007 POISSON 0.17 DENSITY 23.5616 ALPHA 1e-005 DAMP 0.05 TYPE CONCRETE STRENGTH FCU 40000 G 9.28139e+006 ISOTROPIC STEEL E 2.05e+008 POISSON 0.3 DENSITY 76.8195 ALPHA 1.2e-005 DAMP 0.03 TYPE STEEL END DEFINE MATERIAL MEMBER PROPERTY INDIAN 5169 TABLE ST TUBE TH 0.0036 WT 0.1 DT 0.2 CONSTANTS MATERIAL STEEL ALL *85 TO 97 101 TO 103 127 135 136 139 START MY MZ *85 TO 97 101 TO 103 127 135 136 139 END MY MZ *27 106 TO 120 122 123 128 TO 131 133 134 2148 2151 2152 2155 2159 - *2635 START MY MZ *143 156 172 189 389 517 568 625 714 806 890 980 997 1407 1511 1614 1657 1700 - *1746 1855 2004 2111 2182 2276 2365 2456 2540 2657 2741 END MY MZ SUPPORTS 472 2283 PINNED **************** LOAD 1 LOADTYPE Seismic TITLE EQ+X *1893 LOAD X 1 *PERFORM ANALYSIS *CHANGE ******************************************* LOAD 2 LOADTYPE Seismic TITLE EQ+Z *1893 LOAD Z 1 *PERFORM ANALYSIS *CHANGE ************** LOAD 3 LOADTYPE Dead TITLE SELF WT. SELFWEIGHT Y -1 LOAD 4 LOADTYPE Dead TITLE DL OF ROOF SHEETING ****SHEETING LOAD = 0.35KN/M2 ****TRIB = 1.45M MEMBER LOAD 5169 UNI GY -0.5075 *************** LOAD 5 LOADTYPE Dead TITLE SERVICES ****SERVICES = 0.50KN/M2 ****TRIB = 1.45M MEMBER LOAD 5169 UNI GY -0.725 *************** LOAD 6 LOADTYPE Live TITLE ROOF LIVE LOAD ****SERVICES = 0.75KN/M2 ****TRIB = 1.45M MEMBER LOAD 5169 UNI GY -1.09 *************** LOAD 7 LOADTYPE Wind TITLE WIND PRESSURE ****WIND INTENSITY = 4.5KN/M2 ****TRIB = 1.45M MEMBER LOAD 5169 UNI Y 6.525 *************** LOAD 8 LOADTYPE Wind TITLE WIND SUCTION ****WIND INTENSITY = 3KN/M2 ****TRIB = 1.45M MEMBER LOAD 5169 UNI Y 4.35 *************** ****************** ****************** LOAD COMB 101 DL 3 1.0 4 1.0 5 1.0 ****************** LOAD COMB 102 DL+LL 3 1.0 4 1.0 5 1.0 6 1.0 * ********************************** LOAD COMB 103 (DL+EL(X)) 3 1.0 4 1.0 5 1.0 1 1.0 ******************************** LOAD COMB 104 (DL+EL(-X)) 3 1.0 4 1.0 5 1.0 1 -1.0 ******************************* LOAD COMB 105 (DL+EL((Z)) 3 1.0 4 1.0 5 1.0 2 1.0 ****************************** LOAD COMB 106 (DL+EL(-Z)) 3 1.0 4 1.0 5 1.0 2 -1.0 ********************************** LOAD COMB 107 (DL+WLP) 3 1.0 4 1.0 5 1.0 7 1.0 ************************** LOAD COMB 108 (DL+WLS) 3 1.0 4 1.0 5 1.0 8 1.0 ********************************* LOAD COMB 109 DL+0.8(LL)+0.8(ELX) 3 1.0 4 1.0 5 1.0 6 0.8 1 0.8 *************************** LOAD COMB 110 DL+0.8(LL)-0.8(ELX) 3 1.0 4 1.0 5 1.0 6 0.8 1 -0.8 ***************************** LOAD COMB 111 DL+0.8(LL)+0.8(ELZ) 3 1.0 4 1.0 5 1.0 6 0.8 2 0.8 ******************************* LOAD COMB 112 DL+0.8(LL)-0.8(ELZ) 3 1.0 4 1.0 5 1.0 6 0.8 2 -0.8 ********************************** LOAD COMB 113 DL+0.8(LL)+0.8(WXP) 3 1.0 4 1.0 5 1.0 6 0.8 7 0.8 ********************************** LOAD COMB 114 DL+0.8(LL)+0.8(WXS) 3 1.0 4 1.0 5 1.0 6 0.8 8 0.8 ********************************** *LOAD COMB 115 DL+TEMP+ *3 1.0 4 1.0 5 1.0 13 1.0 *********************************** *LOAD COMB 116 DL+TEMP- *3 1.0 4 1.0 5 1.0 13 -1.0 *********************************** *LOAD COMB 117 DL+0.8(LL)+0.8(TEMP+) *3 1.0 4 1.0 5 1.0 6 0.8 13 0.8 *********************************** *LOAD COMB 118 DL+0.8(LL)+0.8(TEMP)- *3 1.0 4 1.0 5 1.0 6 0.8 13 -0.8 **************************** LOAD COMB 119 SW+0.9(DL)+0.9(WLP) 3 1.0 4 0.9 7 0.9 **************************** LOAD COMB 120 SW+0.9(DL)+0.9(WLS) 3 1.0 4 0.9 8 0.9 **************************** PERFORM ANALYSIS DEFINE ENVELOPE 101 TO 114 119 120 ENVELOPE 1 TYPE STRENGTH END DEFINE ENVELOPE LOAD LIST 101 TO 114 119 120 PARAMETER 1 CODE IS800 WSD MAIN 180 ALL FYLD 310000 ALL STP 1 ALL TRACK 0 ALL LY 6 ALL LZ 6 ALL KZ 1 ALL **** **** DFF 300 ALL * CHECK CODE ALL STEEL MEMBER TAKE OFF ALL FINISH
Your inputs in this regard would be extremely helpful.
- The deflection check is not performing for the attached file
- The critical load case number is not showing correct one in the attached fileBelow queries not related to attached staad model
- Can we define any material with the composite section like a concrete column with inscribed I sections (we have done but we cannot get the UC ratios while defining the material through the section wizard)
- When we doing a big building the parameters, material properties are dividing itself. Is there any way to increase the capacity of the file as we set NL for the individual load case.
Also be noted we are using the 20.07.11.33 version