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1. Geometric input for Wind load
Length of Truss structure normal to wind direction 16.2 m at bottom 15 m at the top
Length of Truss structure along the wind direction 17 m
Height of Truss structure 11.16 m 36.614 ft
Foundation level 2 m 6.562 ft
Height above Ground of Truss z = 13.16 m 43.176 ft
2.a For Wind Load defination parameters
Terrain categories: 3 C Surface Roughness
Building/Structure Classes: IV C Exposure condition
Type of Structures 1.15 for 47.220 m/s IV Building Category
2.b Velocity pressure: As per ASCE-2005
Velocity pressure is calculated as
qz= 0.00256 KzKztKdV I (lb/f t )
where V is basic wind speed, I is important factor, Kdis wind directionality factor,
Kzt is topographic factor, and Kz is velocity pressure exposure coefficient. Velocity pressure exposure
factors are listed Table 6-3 of ASCE 7-02 or can be calculated as
Kz= 2.01 (z/zg)2/a
. 1.061
z is height above ground, z shall not be less than 15 ft. except that z shall not be less than 30 ftfor exposure B for low rise building and for component and cladding. a and zg are taken as follows:
Exposure a zg (ft)
B 7 1200
C 9.5 900
D 11.5 700
Topographic Factor,
Kzt= (1+K1+K2+K3)2 No hill, ridge or escarpment
where K1, K2, K3are determined from Figure 6-4 of ASCE 7-02 based on hill, ridge or escarpment.
3. For Earthquake load defination
from Table 6 of ASCE-07-2009SDS 0.4919 Site Class 4 SD1 0.2834 S1 0.216
RF= 7 OMRF
I= 1.5 Important Structure
DT= depth of foundation below soil 1 m
4. Load Combination as per ASCE-07-2009
4 1. 1.4DL
4 2. 1.2DL+ 1.6LL
4 3. 1.2DL+ 1.6Wind+X+LL
4 4. 1.2DL+ 1.6Wind+Z+LL
4 5. 1.2DL+ 1.6Wind-X+LL
4 6. 1.2DL+ 1.6Wind-Z+LL
4 7. 1.2DL+ EQ+Z+LL
4 8. 1.2DL+ EQ+X+LL
4 9. 0.9DL+1.6 Wind+X
4 10. 0.9DL+1.6Wind+Z
4 11. 0.9DL+1.6Wind-X
4 12. 0.9DL+ 1.6Wind-Z
4 12. 0.9DL+ EQ+Z
4 12. 0.9DL+EQ+X
As per IS 1893 part 3 Equivalent for ASCE -07
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 1 of 33STAAD.Pro for Windows Release 2006
Job Information Engineer Checked Approved
Name: Prakash
Date: 30-Jul-14
Comments
Steel Roof Sections
Structure Type SPACE FRAME
Number of Nodes 181 Highest Node 185
Number of Elements 351 Highest Beam 352
Number of Basic Load Cases 4
Number of Combination Load Cases 6
Included in this printout are data for:
All The Whole Structure
Included in this printout are results for load cases:
Type L/C Name
Primary 1 WIND+Z
Primary 2 WIND-Z
Primary 3 DL
Primary 4 LL
Combination 5 1.4DL
Combination 6 1.2DL+1.6L
Combination 7 1.2DL+1.6WIND+Z+L
Combination 8 1.2DL+1.6WIND-Z+L
Combination 9 0.9DL+1.6WIND+Z
Combination 10 0.9DL+1.6WIND-Z
NodesNode X
(m)
Y
(m)
Z
(m)
1 0.000 0.000 0.000
2 5.400 0.000 0.000
3 10.800 0.000 0.000
4 16.200 0.000 0.000
5 0.000 0.000 5.680
6 5.400 0.000 5.680
7 10.800 0.000 5.680
8 16.200 0.000 5.680
9 0.000 0.000 11.320
10 5.400 0.000 11.320
11 10.800 0.000 11.320
12 16.200 0.000 11.320
13 0.000 0.000 17.000
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Roof Design of RCMC
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Nodes Cont...Node X
(m)
Y
(m)
Z
(m)
14 5.400 0.000 17.000
15 10.800 0.000 17.000
16 16.200 0.000 17.000
17 19.800 0.000 0.000
18 19.800 0.000 5.680
19 16.200 0.000 8.500
20 19.800 0.000 8.500
21 0.000 1.000 0.000
22 5.400 1.000 0.00023 10.800 1.000 0.000
24 16.200 1.000 0.000
25 0.000 1.000 5.680
26 5.400 1.000 5.680
27 10.800 1.000 5.680
28 16.200 1.000 5.680
29 0.000 1.000 11.320
30 5.400 1.000 11.320
31 10.800 1.000 11.320
32 16.200 1.000 11.320
33 0.000 1.000 17.000
34 5.400 1.000 17.000
35 10.800 1.000 17.000
36 16.200 1.000 17.000
37 19.800 1.000 0.000
38 19.800 1.000 5.680
39 16.200 1.000 8.500
40 19.800 1.000 8.500
41 0.000 2.000 0.000
42 5.400 2.000 0.000
43 10.800 2.000 0.000
44 16.200 2.000 0.000
45 0.000 2.000 5.680
46 5.400 2.000 5.680
47 10.800 2.000 5.68048 16.200 2.000 5.680
49 0.000 2.000 11.320
50 5.400 2.000 11.320
51 10.800 2.000 11.320
52 16.200 2.000 11.320
53 0.000 2.000 17.000
54 5.400 2.000 17.000
55 10.800 2.000 17.000
56 16.200 2.000 17.000
57 19.800 2.000 0.000
58 19.800 2.000 5.680
59 16.200 2.000 8.500
60 19.800 2.000 8.500
61 0.000 5.300 0.000
62 5.400 5.300 0.000
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Roof Design of RCMC
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Prakash 30-Jul-14
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Print Time/Date: 30/07/2014 17:11 Print Run 3 of 33STAAD.Pro for Windows Release 2006
Nodes Cont...Node X
(m)
Y
(m)
Z
(m)
63 10.800 5.300 0.000
64 16.200 5.300 0.000
65 0.000 5.300 5.680
66 5.400 5.300 5.680
67 10.800 5.300 5.680
68 16.200 5.300 5.680
69 0.000 5.300 11.320
70 5.400 5.300 11.320
71 10.800 5.300 11.32072 16.200 5.300 11.320
73 0.000 5.300 17.000
74 5.400 5.300 17.000
75 10.800 5.300 17.000
76 16.200 5.300 17.000
77 19.800 5.300 0.000
78 19.800 5.300 5.680
79 16.200 5.300 8.500
80 19.800 5.300 8.500
81 0.000 8.600 0.000
82 5.400 8.600 0.000
83 10.800 8.600 0.000
84 16.200 8.600 0.000
85 0.000 8.600 5.680
86 5.400 8.600 5.680
87 10.800 8.600 5.680
88 16.200 8.600 5.680
89 0.000 8.600 11.320
90 5.400 8.600 11.320
91 10.800 8.600 11.320
92 16.200 8.600 11.320
93 0.000 8.600 17.000
94 5.400 8.600 17.000
95 10.800 8.600 17.000
96 16.200 8.600 17.00097 19.800 8.600 0.000
98 19.800 8.600 5.680
99 16.200 8.600 8.500
100 19.800 8.600 8.500
101 16.200 3.650 0.000
102 19.800 3.650 0.000
103 16.200 6.950 0.000
104 19.800 6.950 0.000
105 0.000 8.820 0.000
106 5.400 8.820 0.000
107 10.800 8.820 0.000
108 16.200 8.820 0.000
109 0.000 10.378 5.680
110 5.400 10.378 5.680
111 10.800 10.378 5.680
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Roof Design of RCMC
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Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 4 of 33STAAD.Pro for Windows Release 2006
Nodes Cont...Node X
(m)
Y
(m)
Z
(m)
112 16.200 10.378 5.680
117 0.000 8.820 17.000
118 5.400 8.820 17.000
119 10.800 8.820 17.000
120 16.200 8.820 17.000
121 0.000 8.459 18.295
122 5.400 8.459 18.295
123 10.800 8.459 18.295
124 16.200 8.459 18.295125 0.000 10.378 11.320
126 5.400 10.378 11.320
127 10.800 10.378 11.320
128 16.200 10.378 11.320
129 0.000 11.155 8.494
130 5.400 11.155 8.494
131 10.800 11.155 8.494
132 16.200 11.155 8.494
133 0.000 8.459 -1.307
134 5.400 8.459 -1.307
135 10.800 8.459 -1.307
136 16.200 8.459 -1.307
137 0.000 9.132 1.136
138 0.000 9.443 2.272
139 0.000 9.755 3.408
140 0.000 10.066 4.544
141 0.000 10.066 12.456
142 0.000 9.755 13.592
143 0.000 9.443 14.728
144 0.000 9.132 15.864
145 5.400 9.132 1.136
146 5.400 9.443 2.272
147 5.400 9.755 3.408
148 5.400 10.066 4.544
149 5.400 10.066 12.456150 5.400 9.755 13.592
151 5.400 9.443 14.728
152 5.400 9.132 15.864
153 10.800 9.132 1.136
154 10.800 9.443 2.272
155 10.800 9.755 3.408
156 10.800 10.066 4.544
157 10.800 10.066 12.456
158 10.800 9.755 13.592
159 10.800 9.443 14.728
160 10.800 9.132 15.864
161 16.200 9.132 1.136
162 16.200 9.443 2.272
163 16.200 9.755 3.408
164 16.200 10.066 4.544
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 5 of 33STAAD.Pro for Windows Release 2006
Nodes Cont...Node X
(m)
Y
(m)
Z
(m)
165 16.200 10.066 12.456
166 16.200 9.755 13.592
167 16.200 9.443 14.728
168 16.200 9.132 15.864
169 0.000 10.637 6.618
170 0.000 10.896 7.556
171 0.000 10.896 9.436
172 0.000 10.637 10.378
173 5.400 10.637 6.618174 5.400 10.896 7.556
175 5.400 10.896 9.436
176 5.400 10.637 10.378
177 10.800 10.637 6.618
178 10.800 10.896 7.556
179 10.800 10.896 9.436
180 10.800 10.637 10.378
181 16.200 10.637 6.618
182 16.200 10.896 7.556
183 16.200 10.896 9.436
184 16.200 10.637 10.378
185 0.000 1.000 8.500
BeamsBeam Node A Node B Length
(m)
Property
(degrees)
1 1 21 1.000 1 0
2 2 22 1.000 2 0
3 3 23 1.000 2 0
4 4 24 1.000 1 0
5 17 37 1.000 1 0
6 5 25 1.000 2 0
7 6 26 1.000 2 0
8 7 27 1.000 2 0
9 8 28 1.000 2 0
10 18 38 1.000 1 0
11 9 29 1.000 2 0
12 10 30 1.000 2 0
13 11 31 1.000 2 0
14 19 39 1.000 1 0
15 20 40 1.000 1 0
16 13 33 1.000 1 0
17 14 34 1.000 2 0
18 15 35 1.000 2 0
19 16 36 1.000 1 0
20 12 32 1.000 2 021 21 22 5.400 4 0
22 22 23 5.400 4 0
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 6 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
23 23 24 5.400 4 0
24 24 37 3.600 4 0
25 25 26 5.400 4 0
26 26 27 5.400 4 0
27 27 28 5.400 4 0
28 28 38 3.600 4 0
29 29 30 5.400 4 0
30 30 31 5.400 4 0
31 31 32 5.400 4 032 33 34 5.400 4 0
33 34 35 5.400 4 0
34 35 36 5.400 4 0
35 21 25 5.680 4 0
36 25 185 2.820 4 0
37 29 33 5.680 4 0
38 22 26 5.680 4 0
39 26 30 5.640 4 0
40 30 34 5.680 4 0
41 23 27 5.680 4 0
42 27 31 5.640 4 0
43 31 35 5.680 4 0
44 24 28 5.680 4 0
45 28 39 2.820 4 0
46 39 32 2.820 4 0
47 32 36 5.680 4 0
48 37 38 5.680 4 0
49 38 40 2.820 4 0
50 39 40 3.600 4 0
51 21 41 1.000 1 0
52 22 42 1.000 2 0
53 23 43 1.000 2 0
54 24 44 1.000 1 0
55 25 45 1.000 2 0
56 26 46 1.000 2 057 27 47 1.000 2 0
58 28 48 1.000 2 0
59 29 49 1.000 2 0
60 30 50 1.000 2 0
61 31 51 1.000 2 0
62 32 52 1.000 2 0
63 33 53 1.000 1 0
64 34 54 1.000 2 0
65 35 55 1.000 2 0
66 36 56 1.000 1 0
67 37 57 1.000 1 0
68 38 58 1.000 1 0
69 39 59 1.000 1 0
70 40 60 1.000 1 0
71 41 42 5.400 4 0
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 7 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
72 42 43 5.400 4 0
73 43 44 5.400 4 0
74 44 57 3.600 4 0
75 45 46 5.400 4 0
76 46 47 5.400 4 0
77 47 48 5.400 4 0
78 48 58 3.600 4 0
79 49 50 5.400 4 0
80 50 51 5.400 4 081 51 52 5.400 4 0
82 53 54 5.400 4 0
83 54 55 5.400 4 0
84 55 56 5.400 4 0
85 41 45 5.680 4 0
86 45 49 5.640 4 0
87 49 53 5.680 4 0
88 42 46 5.680 4 0
89 46 50 5.640 4 0
90 50 54 5.680 4 0
91 43 47 5.680 4 0
92 47 51 5.640 4 0
93 51 55 5.680 4 0
94 44 48 5.680 4 0
95 48 59 2.820 4 0
96 59 52 2.820 4 0
97 52 56 5.680 4 0
98 57 58 5.680 4 0
99 58 60 2.820 4 0
100 59 60 3.600 4 0
101 41 61 3.300 1 0
102 42 62 3.300 2 0
103 43 63 3.300 2 0
104 44 101 1.650 1 0
105 45 65 3.300 2 0106 46 66 3.300 2 0
107 47 67 3.300 2 0
108 48 68 3.300 2 0
109 49 69 3.300 2 0
110 50 70 3.300 2 0
111 51 71 3.300 2 0
112 52 72 3.300 2 0
113 53 73 3.300 1 0
114 54 74 3.300 2 0
115 55 75 3.300 2 0
116 56 76 3.300 1 0
117 57 102 1.650 1 0
118 58 78 3.300 1 0
119 59 79 3.300 1 0
120 60 80 3.300 1 0
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 8 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
121 61 62 5.400 3 0
122 62 63 5.400 3 0
123 63 64 5.400 3 0
125 65 66 5.400 3 0
126 66 67 5.400 3 0
127 67 68 5.400 3 0
128 68 78 3.600 3 0
129 69 70 5.400 3 0
130 70 71 5.400 3 0131 71 72 5.400 3 0
132 73 74 5.400 3 0
133 74 75 5.400 3 0
134 75 76 5.400 3 0
135 61 65 5.680 3 0
136 65 69 5.640 3 0
137 69 73 5.680 3 0
138 62 66 5.680 3 0
139 66 70 5.640 3 0
140 70 74 5.680 3 0
141 63 67 5.680 3 0
142 67 71 5.640 3 0
143 71 75 5.680 3 0
144 64 68 5.680 3 0
145 68 79 2.820 3 0
146 79 72 2.820 3 0
147 72 76 5.680 3 0
148 77 78 5.680 3 0
149 78 80 2.820 3 0
150 79 80 3.600 3 0
151 61 81 3.300 1 0
152 62 82 3.300 2 0
153 63 83 3.300 2 0
154 64 103 1.650 1 0
155 65 85 3.300 2 0156 66 86 3.300 2 0
157 67 87 3.300 2 0
158 68 88 3.300 2 0
159 69 89 3.300 2 0
160 70 90 3.300 2 0
161 71 91 3.300 2 0
162 72 92 3.300 2 0
163 73 93 3.300 1 0
164 74 94 3.300 2 0
165 75 95 3.300 2 0
166 76 96 3.300 1 0
167 77 104 1.650 1 0
168 78 98 3.300 1 0
169 79 99 3.300 1 0
170 80 100 3.300 1 0
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 9 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
171 81 82 5.400 5 0
172 82 83 5.400 5 0
173 83 84 5.400 5 0
174 84 97 3.600 5 0
175 85 86 5.400 5 0
176 86 87 5.400 5 0
177 87 88 5.400 5 0
178 88 98 3.600 5 0
179 89 90 5.400 5 0180 90 91 5.400 5 0
181 91 92 5.400 5 0
182 93 94 5.400 5 0
183 94 95 5.400 5 0
184 95 96 5.400 5 0
185 81 85 5.680 5 0
186 85 89 5.640 5 0
187 89 93 5.680 5 0
188 82 86 5.680 5 0
189 86 90 5.640 5 0
190 90 94 5.680 5 0
191 83 87 5.680 5 0
192 87 91 5.640 5 0
193 91 95 5.680 5 0
194 84 88 5.680 5 0
195 88 99 2.820 5 0
196 99 92 2.820 5 0
197 92 96 5.680 5 0
198 97 98 5.680 5 0
199 98 100 2.820 5 0
200 99 100 3.600 5 0
201 101 64 1.650 1 0
202 102 77 1.650 1 0
203 103 84 1.650 1 0
204 104 97 1.650 1 0205 101 102 3.600 3 0
206 103 104 3.600 3 0
207 81 105 0.220 1 0
208 82 106 0.220 2 0
209 83 107 0.220 2 0
210 84 108 0.220 1 0
211 93 117 0.220 1 0
212 94 118 0.220 2 0
213 95 119 0.220 2 0
214 96 120 0.220 1 0
215 85 109 1.778 2 0
216 86 110 1.778 2 0
217 87 111 1.778 2 0
218 88 112 1.778 2 0
219 89 125 1.778 2 0
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 10 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
220 90 126 1.778 2 0
221 91 127 1.778 2 0
222 92 128 1.778 2 0
223 105 137 1.178 5 0
224 109 169 0.973 5 0
225 129 171 0.977 5 0
226 125 141 1.178 5 0
227 117 121 1.344 5 0
228 106 145 1.178 7 0229 110 173 0.973 7 0
230 130 175 0.977 7 0
231 126 149 1.178 7 0
232 118 122 1.344 7 0
233 107 153 1.178 7 0
234 111 177 0.973 7 0
235 131 179 0.977 7 0
236 127 157 1.178 7 0
237 119 123 1.344 7 0
238 108 161 1.178 5 0
239 112 181 0.973 5 0
240 132 183 0.977 5 0
241 128 165 1.178 5 0
242 120 124 1.344 5 0
243 133 105 1.356 5 0
244 134 106 1.356 7 0
245 135 107 1.356 7 0
246 136 108 1.356 5 0
247 109 110 5.400 6 0
248 110 111 5.400 6 0
249 111 112 5.400 6 0
250 129 130 5.400 6 0
251 130 131 5.400 6 0
252 131 132 5.400 6 0
253 125 126 5.400 6 0254 126 127 5.400 6 0
255 127 128 5.400 6 0
256 137 138 1.178 5 0
257 138 139 1.178 5 0
258 139 140 1.178 5 0
259 140 109 1.178 5 0
260 141 142 1.178 5 0
261 142 143 1.178 5 0
262 143 144 1.178 5 0
263 144 117 1.178 5 0
264 145 146 1.178 7 0
265 146 147 1.178 7 0
266 147 148 1.178 7 0
267 148 110 1.178 7 0
268 149 150 1.178 7 0
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 11 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
269 150 151 1.178 7 0
270 151 152 1.178 7 0
271 152 118 1.178 7 0
272 153 154 1.178 7 0
273 154 155 1.178 7 0
274 155 156 1.178 7 0
275 156 111 1.178 7 0
276 157 158 1.178 7 0
277 158 159 1.178 7 0278 159 160 1.178 7 0
279 160 119 1.178 7 0
280 161 162 1.178 5 0
281 162 163 1.178 5 0
282 163 164 1.178 5 0
283 164 112 1.178 5 0
284 165 166 1.178 5 0
285 166 167 1.178 5 0
286 167 168 1.178 5 0
287 168 120 1.178 5 0
288 169 170 0.973 5 0
289 170 129 0.973 5 0
290 171 172 0.977 5 0
291 172 125 0.977 5 0
292 173 174 0.973 7 0
293 174 130 0.973 7 0
294 175 176 0.977 7 0
295 176 126 0.977 7 0
296 177 178 0.973 7 0
297 178 131 0.973 7 0
298 179 180 0.977 7 0
299 180 127 0.977 7 0
300 181 182 0.973 5 0
301 182 132 0.973 5 0
302 183 184 0.977 5 0303 184 128 0.977 5 0
304 133 134 5.400 6 0
305 134 135 5.400 6 0
306 135 136 5.400 6 0
307 105 106 5.400 6 0
308 106 107 5.400 6 0
309 107 108 5.400 6 0
310 137 145 5.400 6 0
311 145 153 5.400 6 0
312 153 161 5.400 6 0
313 138 146 5.400 6 0
314 146 154 5.400 6 0
315 154 162 5.400 6 0
316 139 147 5.400 6 0
317 147 155 5.400 6 0
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12
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 12 of 33STAAD.Pro for Windows Release 2006
Beams Cont...Beam Node A Node B Length
(m)
Property
(degrees)
318 155 163 5.400 6 0
319 140 148 5.400 6 0
320 148 156 5.400 6 0
321 156 164 5.400 6 0
322 169 173 5.400 6 0
323 173 177 5.400 6 0
324 177 181 5.400 6 0
325 170 174 5.400 6 0
326 174 178 5.400 6 0327 178 182 5.400 6 0
328 171 175 5.400 6 0
329 175 179 5.400 6 0
330 179 183 5.400 6 0
331 172 176 5.400 6 0
332 176 180 5.400 6 0
333 180 184 5.400 6 0
334 141 149 5.400 6 0
335 149 157 5.400 6 0
336 157 165 5.400 6 0
337 142 150 5.400 6 0
338 150 158 5.400 6 0
339 158 166 5.400 6 0
340 143 151 5.400 6 0
341 151 159 5.400 6 0
342 159 167 5.400 6 0
343 144 152 5.400 6 0
344 152 160 5.400 6 0
345 160 168 5.400 6 0
346 117 118 5.400 6 0
347 118 119 5.400 6 0
348 119 120 5.400 6 0
349 121 122 5.400 6 0
350 122 123 5.400 6 0
351 123 124 5.400 6 0352 185 29 2.820 4 0
Section PropertiesProp Section Area
(cm2)
Iyy
(cm4)
Izz
(cm4)
J
(cm4)
Material
1 Rect 0.40x0.40 1.6E 3 213E 3 213E 3 360E 3 M25
2 Rect 0.60x0.60 3.6E 3 1.08E 6 1.08E 6 1.82E 6 M25
3 Rect 0.60x0.30 1.8E 3 135E 3 540E 3 371E 3 M20
4 Rect 0.45x0.30 1.35E 3 101E 3 228E 3 238E 3 M20
5 Rect 0.50x0.30 1.5E 3 113E 3 313E 3 282E 3 M20
6 ISMC100 23.400 304.650 373.400 3.453 STEEL7 ISLC200 52.440 1.64E 3 3.45E 3 14.696 STEEL
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 13 of 33STAAD.Pro for Windows Release 2006
MaterialsMat Name E
(kN/mm2)
Density
(kg/m3)
(1/K)
1 M20 22.360 0.170 2.5E 3 11E -6
2 STEEL 205.000 0.300 7.83E 3 12E -6
3 M25 25.000 0.170 2.5E 3 11E -6
4 ALUMINUM 68.948 0.330 2.71E 3 23E -6
5 CONCRETE 21.718 0.170 2.4E 3 10E -6
Basic Load Cases
Number Name
1 WIND+Z
2 WIND-Z
3 DL
4 LL
Combination Load CasesComb. Combination L/C Name Primary Primary L/C Name Factor
5 1.4DL 3 DL 1.40
6 1.2DL+1.6L 3 DL 1.20
4 LL 1.60
7 1.2DL+1.6WIND+Z+L 3 DL 1.20
1 WIND+Z 1.60
4 LL 1.00
8 1.2DL+1.6WIND-Z+L 3 DL 1.20
1 WIND+Z 1.60
4 LL 1.00
9 0.9DL+1.6WIND+Z 3 DL 0.90
1 WIND+Z 1.60
10 0.9DL+1.6WIND-Z 3 DL 0.90
2 WIND-Z 1.60
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 15 of 33STAAD.Pro for Windows Release 2006
-0.150 kN/m-0.150 kN/m
-0.150 kN/m
-0.150 kN/m
-0.150 kN/m-0.150 kN/m
-0.250 kN/m-0.250 kN/m -0.250 kN/m
-0.250 kN/m-0.250 kN/m -0.250 kN/m
-0.200 kN/m-0.200 kN/m
-0.200 kN/m-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m -0.200 kN/m-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m-0.200 kN/m -0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m -0.200 kN/m
-0.200 kN/m
-0.200 kN/m-0.200 kN/m-0.200 kN/m
Load 5
XY
Z
Loads on Roof Purlins (Input data was modified after picture taken)
-0.670 kN/m-0.670 kN/m
-0.670 kN/m
-0.670 kN/m
-0.670 kN/m-0.670 kN/m
-1.275 kN/m-1.275 kN/m -1.275 kN/m
-1.275 kN/m-1.275 kN/m -1.275 kN/m
-1.180 kN/m-1.180 kN/m
-1.180 kN/m-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m -1.180 kN/m-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m-1.180 kN/m -1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m -1.180 kN/m
-1.180 kN/m
-1.180 kN/m-1.180 kN/m-1.180 kN/m
Load 6
XY
Z
Live load on Roof (Input data was modified after picture taken)
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 16 of 33STAAD.Pro for Windows Release 2006
3D Rendered View (Input data was modified after picture taken)
0.3910.715
0.1930.625
0.3920.6
0.465
0.6760.328
0.196
0.628
0.625
0.392
0.327
0.601
0.646
0.455
0.732
0.323
0.328
0.677
0.614
0.628
0.563
0.636
0.3270.646
0.393
0.463
0.621
0.3230.652
0.189
0.693
0.6260.566
0.6220.633
0.185
0.638
0.6480.393
0.1850.626
0.6830.19
0.684
0.19
0.674
0.649
0.3930.626
0.637
0.185
0.626
0.5640.634
0.186
0.463
0.465
0.323
0.6540.19
0.628
0.327
0.693
0.6480.393
0.731
0.621
0.328
0.615
0.5650.637
0.394
0.599
0.609
0.323
0.684
0.193
0.627
0.327
0.649
0.505
0.328
0.626
0.393
0.599
0.464
0.193
0.629
0.731
0.393
X
Y
Whole Structure-3D Passed Section Steel Check (Input data was modified after picture taken)
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 17 of 33STAAD.Pro for Windows Release 2006
ISMC100:0.391
ISMC100:0.715
ISLC200:0.193
ISMC100:0.392
ISMC100:0.625
ISLC200:0.6
ISMC100:0.676
ISLC200:0.196
ISMC100:0.392
ISMC100:0.465
ISLC200:0.328
ISMC100:0.625
ISLC200:0.601
ISMC100:0.732
ISMC100:0.628
ISLC200:0.327
ISMC100:0.455
ISLC200:0.328
ISMC100:0.628
ISMC100:0.646
ISLC200:0.323
ISMC100:0.614
ISLC200:0.327
ISMC100:0.463
ISMC100:0.677
ISLC200:0.563
ISMC100:0.646
ISLC200:0.323
ISMC100:0.636
ISMC100:0.626
ISLC200:0.393
ISMC100:0.652
ISMC100:0.621
ISLC200:0.566
ISMC100:0.648
ISLC200:0.189
ISMC100:0.633
ISMC100:0.693
ISLC200:0.393
ISLC200:0.185
ISMC100:0.684
ISMC100:0.622ISMC100:0.626
ISLC200:0.19
ISLC200:0.185
ISMC100:0.638ISMC100:0.637
ISMC100:0.674
ISLC200:0.19
ISMC100:0.683
ISLC200:0.185
ISMC100:0.626ISMC100:0.465
ISLC200:0.393
ISMC100:0.649
ISLC200:0.186
ISMC100:0.634
ISLC200:0.564
ISMC100:0.693
ISLC200:0.19
ISMC100:0.626
ISMC100:0.654
ISMC100:0.621
ISLC200:0.323
ISLC200:0.393
ISMC100:0.463
ISMC100:0.648
ISMC100:0.637
ISLC200:0.327
ISLC200:0.565
ISMC100:0.628
ISMC100:0.615
ISMC100:0.684
ISLC200:0.328
ISLC200:0.323
ISMC100:0.731
ISMC100:0.609
ISMC100:0.649
ISLC200:0.599
ISLC200:0.327
ISMC100:0.627
ISMC100:0.394
ISMC100:0.626
ISLC200:0.193
ISLC200:0.328
ISMC100:0.505
ISMC100:0.464
ISLC200:0.599ISMC100:0.629
ISMC100:0.393ISLC200:0.193ISMC100:0.731
ISMC100:0.393
Load 1
XY
Z
Passed Steel section check for Roof (Input data was modified after picture taken)
Bending ZBeam Stress :Load 7 :
XY
Z
Whole Structure Mz 100kNm:1m Beam Stress 5e+008mm:m 7 1.2DL+1.6WIND+Z+L
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19
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 19 of 33STAAD.Pro for Windows Release 2006
Design Of Member No. 1 As Per IS:800
Input Parameters
Member Section 2XISLC200
- 0 mm face-to-face
Cross Sectional Area Ax(m2) 0.01
Shear Area Along Major Axis Az(m2) 0.00
Shear Area Along Minor Axis Ay(m2) 0.00
rz(m ) 0.08
ry(m ) 0.06
Section Modulus About Major Axis - Tension Edge Stz(m3) 0.00
Section Modulus About Major Axis - Compression Edge Szz(m3) 0.00
Section Modulus About Minor Axis - Tension Edge Sty(m3) 0.00
Section Modulus About Minor Axis - Compression Edge Syy(m3) 0.00
Unsupported Length - Major Axis For Slenderness Check Lz(m ) 2.93
Unsupported Length - Minor Axis For Slenderness Check Ly(m ) 0.98
Effective Length For Allowable Bending Stress Calculation Unl (m ) 0.98
Yield Stress fy(MPa) 250.00
Allowable Ratio For Interaction Check 1.00
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx(kN ) 55.22
Major Axis Moment Mz(kN m ) 17.93
Minor Axis Moment My(kN m ) 0.24
Critical Loadcase No. 6
Critical Section (m ) 0.98
Beam No. 295
Shear Along Major Axis
Shear Along Major Axis Fz(kN ) 0.45
Critical Loadcase No. 6
Critical Section (m ) 0.00
Beam No. 230
Shear Along Minor Axis
Shear Along Minor Axis Fy(kN ) 19.18
Critical Loadcase No. 6
Critical Section (m ) 0.98
Beam No. 295
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 20 of 33STAAD.Pro for Windows Release 2006
Details Of Calculation
Slenderness Checking
Lez(m ) 2.93
Ley(m ) 0.98
Lez/ rz 36.13
Ley/ ry 17.10
Actual Slenderness Ratio 36.13
Allowable Slenderness Ratio 180.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc(MPa)
=Fx/ Ax 10.53
Calculation Of Allowable Compressive Stress :
E (MPa) 200000.00
L / r 36.13
fcc
(MPa)
=2E /
21512.24
Allowable Compressive Stress fc_allowable
(MPa)
=0.6fccfy/ [(fcc)1.4
+ (fy)1.4
] 141.93
Bending about Major Axis :
Actual Bending Compressive Stress - Major Axis fcz
(MPa)
=Mz / Szz 51.96
Calculation of Allowable Bending Stress About Major Axis :
L / r 17.10
Y (MPa)
=26.5 x 105/ (L / r)
29063.19
D / Tf 18.52
X (MPa)
=Y[ 1 + 1/20(( L / r) / (D / T f))2]0.5
9254.36
k1 1.00
k2 0.00
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 21 of 33STAAD.Pro for Windows Release 2006
c1 1.00
c2 1.00
Elastic Critical Stress fcb
(MPa)
=k1(X + k2Y)c2/c1 9254.36
Allowable Bending Compressive Stress - Major Axis fcz_allowable
(MPa)
=0.66fcbfy/ [(fcb)1.4
+ (fy)1.4
]1 / 1.4
164.22
Bending about Minor Axis :
Actual Bending Compressive Stress - Minor Axis fcy
(MPa)
=My / Syy 1.03
Calculation of Allowable Bending Stress About Minor Axis :
Allowable Bending Compressive Stress - Minor Axis fcy_allowable
(MPa)
=0.66fy 165.00
Interaction Checking
Interaction ratio
=fc/ fc_allowable+ fcz/ fcz_allowable+ fcy/ fcy_allowable 0.40
Status SAFE
Check Against Shear
Shear Stress Along Major Axis Vz(MPa)
=Fz/ Az 0.21
Shear Stress Along Minor Axis Vy(MPa)
=Fy/ Ay 8.72
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 100.00
Interaction ratio (Along Major Axis)
=Vz/ V_allowable 0.00
Status SAFE
Interaction ratio (Along Minor Axis)
=Vy/ V_allowable 0.09
Status SAFE
Deflection Checking Ignored
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 22 of 33STAAD.Pro for Windows Release 2006
Design Of Member No. 2 As Per IS:800
Input Parameters
Member Section 2XISLC200
- 0 mm face-to-face
Cross Sectional Area Ax(m2) 0.01
Shear Area Along Major Axis Az(m2) 0.00
Shear Area Along Minor Axis Ay(m2) 0.00
rz(m ) 0.08
ry(m ) 0.06
Section Modulus About Major Axis - Tension Edge Stz(m3) 0.00
Section Modulus About Major Axis - Compression Edge Szz(m3) 0.00
Section Modulus About Minor Axis - Tension Edge Sty(m3) 0.00
Section Modulus About Minor Axis - Compression Edge Syy(m3) 0.00
Unsupported Length - Major Axis For Slenderness Check Lz(m ) 5.89
Unsupported Length - Minor Axis For Slenderness Check Ly(m ) 1.18
Effective Length For Allowable Bending Stress Calculation Unl (m ) 1.18
Yield Stress fy(MPa) 250.00
Allowable Ratio For Interaction Check 1.00
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx(kN ) 49.39
Major Axis Moment Mz(kN m ) 30.26
Minor Axis Moment My(kN m ) -0.02
Critical Loadcase No. 6
Critical Section (m ) 1.18
Beam No. 271
Shear Along Major Axis
Shear Along Major Axis Fz(kN ) 0.15
Critical Loadcase No. 10
Critical Section (m ) 0.00
Beam No. 271
Shear Along Minor Axis
Shear Along Minor Axis Fy(kN ) 25.95
Critical Loadcase No. 6
Critical Section (m ) 1.18
Beam No. 271
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 23 of 33STAAD.Pro for Windows Release 2006
Details Of Calculation
Slenderness Checking
Lez(m ) 5.89
Ley(m ) 1.18
Lez/ rz 72.60
Ley/ ry 20.62
Actual Slenderness Ratio 72.60
Allowable Slenderness Ratio 400.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc(MPa)
=Fx/ Ax 9.42
Calculation Of Allowable Compressive Stress :
E (MPa) 200000.00
L / r 72.60
fcc
(MPa)
=2E /
2374.47
Allowable Compressive Stress fc_allowable
(MPa)
=0.6fccfy/ [(fcc)1.4
+ (fy)1.4
] 108.78
Bending about Major Axis :
Actual Bending Compressive Stress - Major Axis fcz
(MPa)
=Mz / Szz 87.69
Calculation of Allowable Bending Stress About Major Axis :
L / r 20.62
Y (MPa)
=26.5 x 105/ (L / r)
26234.05
D / Tf 18.52
X (MPa)
=Y[ 1 + 1/20(( L / r) / (D / T f))2]0.5
6424.33
k1 1.00
k2 0.00
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24
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 24 of 33STAAD.Pro for Windows Release 2006
c1 1.00
c2 1.00
Elastic Critical Stress fcb
(MPa)
=k1(X + k2Y)c2/c1 6424.33
Allowable Bending Compressive Stress - Major Axis fcz_allowable
(MPa)
=0.66fcbfy/ [(fcb)1.4
+ (fy)1.4
]1 / 1.4
163.73
Bending about Minor Axis :
Actual Bending Compressive Stress - Minor Axis fcy
(MPa)
=My / Syy 0.09
Calculation of Allowable Bending Stress About Minor Axis :
Allowable Bending Compressive Stress - Minor Axis fcy_allowable
(MPa)
=0.66fy 165.00
Interaction Checking
Interaction ratio
=fc/ fc_allowable+ fcz/ fcz_allowable+ fcy/ fcy_allowable 0.62
Status SAFE
Check Against Shear
Shear Stress Along Major Axis Vz(MPa)
=Fz/ Az 0.07
Shear Stress Along Minor Axis Vy(MPa)
=Fy/ Ay 11.80
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 100.00
Interaction ratio (Along Major Axis)
=Vz/ V_allowable 0.00
Status SAFE
Interaction ratio (Along Minor Axis)
=Vy/ V_allowable 0.12
Status SAFE
Deflection Checking Ignored
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25
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 25 of 33STAAD.Pro for Windows Release 2006
Design Of Member No. 3 As Per IS:800
Input Parameters
Member Section 2XISMC100
- 0 mm face-to-face
Cross Sectional Area Ax(m2) 0.00
Shear Area Along Major Axis Az(m2) 0.00
Shear Area Along Minor Axis Ay(m2) 0.00
rz(m ) 0.04
ry(m ) 0.04
Section Modulus About Major Axis - Tension Edge Stz(m3) 0.00
Section Modulus About Major Axis - Compression Edge Szz(m3) 0.00
Section Modulus About Minor Axis - Tension Edge Sty(m3) 0.00
Section Modulus About Minor Axis - Compression Edge Syy(m3) 0.00
Unsupported Length - Major Axis For Slenderness Check Lz(m ) 5.40
Unsupported Length - Minor Axis For Slenderness Check Ly(m ) 5.40
Effective Length For Allowable Bending Stress Calculation Unl (m ) 5.40
Yield Stress fy(MPa) 250.00
Allowable Ratio For Interaction Check 1.00
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx(kN ) 0.03
Major Axis Moment Mz(kN m ) 3.96
Minor Axis Moment My(kN m ) 0.04
Critical Loadcase No. 7
Critical Section (m ) 0.00
Beam No. 340
Shear Along Major Axis
Shear Along Major Axis Fz(kN ) 0.01
Critical Loadcase No. 10
Critical Section (m ) 0.00
Beam No. 340
Shear Along Minor Axis
Shear Along Minor Axis Fy(kN ) 6.35
Critical Loadcase No. 6
Critical Section (m ) 0.00
Beam No. 340
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26
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 26 of 33STAAD.Pro for Windows Release 2006
Details Of Calculation
Slenderness Checking
Lez(m ) 5.40
Ley(m ) 5.40
Lez/ rz 135.18
Ley/ ry 141.99
Actual Slenderness Ratio 141.99
Allowable Slenderness Ratio 400.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc(MPa)
=Fx/ Ax 0.01
Calculation Of Allowable Compressive Stress :
E (MPa) 200000.00
L / r 141.99
fcc
(MPa)
=2E /
297.91
Allowable Compressive Stress fc_allowable
(MPa)
=0.6fccfy/ [(fcc)1.4
+ (fy)1.4
] 49.55
Bending about Major Axis :
Actual Bending Compressive Stress - Major Axis fcz
(MPa)
=Mz / Szz 53.02
Calculation of Allowable Bending Stress About Major Axis :
L / r 141.99
Y (MPa)
=26.5 x 105/ (L / r)
2131.44
D / Tf 13.33
X (MPa)
=Y[ 1 + 1/20(( L / r) / (D / T f))2]0.5
339.48
k1 1.00
k2 0.00
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27
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 27 of 33STAAD.Pro for Windows Release 2006
c1 1.00
c2 1.00
Elastic Critical Stress fcb
(MPa)
=k1(X + k2Y)c2/c1 339.48
Allowable Bending Compressive Stress - Major Axis fcz_allowable
(MPa)
=0.66fcbfy/ [(fcb)1.4
+ (fy)1.4
]1 / 1.4
115.28
Bending about Minor Axis :
Actual Bending Compressive Stress - Minor Axis fcy
(MPa)
=My / Syy 0.61
Calculation of Allowable Bending Stress About Minor Axis :
Allowable Bending Compressive Stress - Minor Axis fcy_allowable
(MPa)
=0.66fy 165.00
Interaction Checking
Interaction ratio
=fc/ fc_allowable+ fcz/ fcz_allowable+ fcy/ fcy_allowable 0.46
Status SAFE
Check Against Shear
Shear Stress Along Major Axis Vz(MPa)
=Fz/ Az 0.01
Shear Stress Along Minor Axis Vy(MPa)
=Fy/ Ay 6.76
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 100.00
Interaction ratio (Along Major Axis)
=Vz/ V_allowable 0.00
Status SAFE
Interaction ratio (Along Minor Axis)
=Vy/ V_allowable 0.07
Status SAFE
Deflection Checking Ignored
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28
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 28 of 33STAAD.Pro for Windows Release 2006
Design Of Member No. 4 As Per IS:800
Input Parameters
Member Section 2XISMC100
- 0 mm face-to-face
Cross Sectional Area Ax(m2) 0.00
Shear Area Along Major Axis Az(m2) 0.00
Shear Area Along Minor Axis Ay(m2) 0.00
rz(m ) 0.04
ry(m ) 0.04
Section Modulus About Major Axis - Tension Edge Stz(m3) 0.00
Section Modulus About Major Axis - Compression Edge Szz(m3) 0.00
Section Modulus About Minor Axis - Tension Edge Sty(m3) 0.00
Section Modulus About Minor Axis - Compression Edge Syy(m3) 0.00
Unsupported Length - Major Axis For Slenderness Check Lz(m ) 5.40
Unsupported Length - Minor Axis For Slenderness Check Ly(m ) 5.40
Effective Length For Allowable Bending Stress Calculation Unl (m ) 5.40
Yield Stress fy(MPa) 250.00
Allowable Ratio For Interaction Check 1.00
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx(kN ) 0.02
Major Axis Moment Mz(kN m ) 5.57
Minor Axis Moment My(kN m ) 0.03
Critical Loadcase No. 6
Critical Section (m ) 0.00
Beam No. 341
Shear Along Major Axis
Shear Along Major Axis Fz(kN ) 0.00
Critical Loadcase No. 9
Critical Section (m ) 0.00
Beam No. 341
Shear Along Minor Axis
Shear Along Minor Axis Fy(kN ) 6.33
Critical Loadcase No. 6
Critical Section (m ) 0.00
Beam No. 341
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29
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 29 of 33STAAD.Pro for Windows Release 2006
Details Of Calculation
Slenderness Checking
Lez(m ) 5.40
Ley(m ) 5.40
Lez/ rz 135.18
Ley/ ry 141.99
Actual Slenderness Ratio 141.99
Allowable Slenderness Ratio 180.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc(MPa)
=Fx/ Ax 0.01
Calculation Of Allowable Compressive Stress :
E (MPa) 200000.00
L / r 141.99
fcc
(MPa)
=2E /
297.91
Allowable Compressive Stress fc_allowable
(MPa)
=0.6fccfy/ [(fcc)1.4
+ (fy)1.4
] 49.55
Bending about Major Axis :
Actual Bending Compressive Stress - Major Axis fcz
(MPa)
=Mz / Szz 74.62
Calculation of Allowable Bending Stress About Major Axis :
L / r 141.99
Y (MPa)
=26.5 x 105/ (L / r)
2131.44
D / Tf 13.33
X (MPa)
=Y[ 1 + 1/20(( L / r) / (D / T f))2]0.5
339.48
k1 1.00
k2 0.00
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30
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 30 of 33STAAD.Pro for Windows Release 2006
c1 1.00
c2 1.00
Elastic Critical Stress fcb
(MPa)
=k1(X + k2Y)c2/c1 339.48
Allowable Bending Compressive Stress - Major Axis fcz_allowable
(MPa)
=0.66fcbfy/ [(fcb)1.4
+ (fy)1.4
]1 / 1.4
115.28
Bending about Minor Axis :
Actual Bending Compressive Stress - Minor Axis fcy
(MPa)
=My / Syy 0.47
Calculation of Allowable Bending Stress About Minor Axis :
Allowable Bending Compressive Stress - Minor Axis fcy_allowable
(MPa)
=0.66fy 165.00
Interaction Checking
Interaction ratio
=fc/ fc_allowable+ fcz/ fcz_allowable+ fcy/ fcy_allowable 0.65
Status SAFE
Check Against Shear
Shear Stress Along Major Axis Vz(MPa)
=Fz/ Az 0.00
Shear Stress Along Minor Axis Vy(MPa)
=Fy/ Ay 6.73
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 100.00
Interaction ratio (Along Major Axis)
=Vz/ V_allowable 0.00
Status SAFE
Interaction ratio (Along Minor Axis)
=Vy/ V_allowable 0.07
Status SAFE
Deflection Checking Ignored
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31
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 31 of 33STAAD.Pro for Windows Release 2006
Design Of Member No. 5 As Per IS:800
Input Parameters
Member Section 2XISMC100
- 0 mm face-to-face
Cross Sectional Area Ax(m2) 0.00
Shear Area Along Major Axis Az(m2) 0.00
Shear Area Along Minor Axis Ay(m2) 0.00
rz(m ) 0.04
ry(m ) 0.04
Section Modulus About Major Axis - Tension Edge Stz(m3) 0.00
Section Modulus About Major Axis - Compression Edge Szz(m3) 0.00
Section Modulus About Minor Axis - Tension Edge Sty(m3) 0.00
Section Modulus About Minor Axis - Compression Edge Syy(m3) 0.00
Unsupported Length - Major Axis For Slenderness Check Lz(m ) 5.40
Unsupported Length - Minor Axis For Slenderness Check Ly(m ) 5.40
Effective Length For Allowable Bending Stress Calculation Unl (m ) 5.40
Yield Stress fy(MPa) 250.00
Allowable Ratio For Interaction Check 1.00
Design Forces
Combined Axial Force & Bi-axial moment
Axial Load Fx(kN ) 0.04
Major Axis Moment Mz(kN m ) 3.96
Minor Axis Moment My(kN m ) 0.06
Critical Loadcase No. 7
Critical Section (m ) 5.40
Beam No. 342
Shear Along Major Axis
Shear Along Major Axis Fz(kN ) 0.02
Critical Loadcase No. 10
Critical Section (m ) 0.00
Beam No. 342
Shear Along Minor Axis
Shear Along Minor Axis Fy(kN ) 6.35
Critical Loadcase No. 6
Critical Section (m ) 5.40
Beam No. 342
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32
Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
Print Time/Date: 30/07/2014 17:11 Print Run 32 of 33STAAD.Pro for Windows Release 2006
Details Of Calculation
Slenderness Checking
Lez(m ) 5.40
Ley(m ) 5.40
Lez/ rz 135.18
Ley/ ry 141.99
Actual Slenderness Ratio 141.99
Allowable Slenderness Ratio 400.00
Status SAFE
Check Against Axial Compression And Bi-Axial Bending
Actual Compressive Stress fc(MPa)
=Fx/ Ax 0.02
Calculation Of Allowable Compressive Stress :
E (MPa) 200000.00
L / r 141.99
fcc
(MPa)
=2E /
297.91
Allowable Compressive Stress fc_allowable
(MPa)
=0.6fccfy/ [(fcc)1.4
+ (fy)1.4
] 49.55
Bending about Major Axis :
Actual Bending Compressive Stress - Major Axis fcz
(MPa)
=Mz / Szz 53.07
Calculation of Allowable Bending Stress About Major Axis :
L / r 141.99
Y (MPa)
=26.5 x 105/ (L / r)
2131.44
D / Tf 13.33
X (MPa)
=Y[ 1 + 1/20(( L / r) / (D / T f))2]0.5
339.48
k1 1.00
k2 0.00
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Roof Design of RCMC
U.S> Army of Corps
Prakash 30-Jul-14
30-Jul-2014 17:05Roof Steel for RCMC.std
c1 1.00
c2 1.00
Elastic Critical Stress fcb
(MPa)
=k1(X + k2Y)c2/c1 339.48
Allowable Bending Compressive Stress - Major Axis fcz_allowable
(MPa)
=0.66fcbfy/ [(fcb)1.4
+ (fy)1.4
]1 / 1.4
115.28
Bending about Minor Axis :
Actual Bending Compressive Stress - Minor Axis fcy
(MPa)
=My / Syy 0.83
Calculation of Allowable Bending Stress About Minor Axis :
Allowable Bending Compressive Stress - Minor Axis fcy_allowable
(MPa)
=0.66fy 165.00
Interaction Checking
Interaction ratio
=fc/ fc_allowable+ fcz/ fcz_allowable+ fcy/ fcy_allowable 0.47
Status SAFE
Check Against Shear
Shear Stress Along Major Axis Vz(MPa)
=Fz/ Az 0.02
Shear Stress Along Minor Axis Vy(MPa)
=Fy/ Ay 6.76
Allowable Shear Stress V_allowable
(MPa)
=0.4fy 100.00
Interaction ratio (Along Major Axis)
=Vz/ V_allowable 0.00
Status SAFE
Interaction ratio (Along Minor Axis)
=Vy/ V_allowable 0.07
Status SAFE
Deflection Checking Ignored