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Analysis Report of Steel Roof of RCMC

Jun 02, 2018

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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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    Analysis of Steel Roof for Reginonal Crisis Management Cen

    Software licensed to HBE

    Job Title

    Client

    Job No Sheet No Rev

    Part

    Ref

    By Date Chd

    File Date/Time

    1

    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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    2

    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 2 of 33STAAD.Pro for Windows Release 2006

    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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    3

    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 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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    4

    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 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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    5

    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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    7

    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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    10

    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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    11

    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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    13

    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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    15

    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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    16

    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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    17

    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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    20

    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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    21

    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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    23

    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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    33

    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