Research Article

Behaviour and Optimization Aids of Composite Stiffened Hypar Shell Roofs with Cutout under Free Vibration

Table 8

Values of “ 𝑟 ” for +45/−45/+45/−45 hypar shells.

Edge condition 𝑦 𝑥
0.20.30.40.50.60.70.8

0.275.577.5279.6281.9179.6277.5375.48
0.377.7383.0988.1390.2287.4883.177.73
0.479.8888.1394.6797.194.6687.779.88
CCCC0.581.6490.2296.1810096.1889.4381.65
0.679.8887.4894.6797.194.6787.5679.88
0.777.7383.187.7890.2387.4583.0977.73
0.875.2377.2479.4681.9179.5977.2675.22

0.2107.37111.09113.43114.35113.44111.12107.33
0.3109.36116.53120.39120.22120.33116.71109.43
0.4110.05113.46112.76111.31112.73113.62110.23
CSCC0.5106.26107.25102.28100102.23107.25106.1
0.6103.13100.6495.5393.2695.47100.66102.59
0.798.4494.1190.948990.8694.9697.47
0.892.8589.9887.1785.7787.1190.0792.03

0.292.2597.51102.65106.18110.36109.26107.52
0.390.3195.06100.71107.15113.38116.61111.43
0.487.3990.9395.43102.23112.88120.74113.94
CCSC0.586.0188.9493.11100111.51120.59114.85
0.687.3990.9395.43102.23112.88120.71113.96
0.790.3195.07100.71107.15113.39116.77111.39
0.892.2297.4102.31106.04110.01109.17107.57

0.291.8690.0287.1485.7887.1490.0291.86
0.397.0994.8590.898990.8994.8597.09
0.4102.26100.6295.593.2795.5100.62102.25
CCCS0.5105.99107.28102.26100102.26107.28105.93
0.6110.5113.49112.73111.27112.72113.49110.06
0.7109.37116.56120.35120.21120.35116.58109.37
0.8106.23109.95112.53113.65112.87110.26106.66

0.295.93100.5103.22102.74101.52100.2297.64
0.393.2897.34101.01102.67103.21102.67100.37
0.490.6194.0197.93100.97102.56103.17101.65
CSSC0.591.1394.498.11100100.55102.33102.63
0.695.0198.53100.0597.7197.28100.34102.78
0.799.07101.1998.1993.9493.3296.5999.91
0.896.6798.4294.3390.3389.6692.3395.22

0.297.1798.6294.3890.4189.8392.6195.51
0.399.04101.4298.1793.9993.4996.79100.11
0.49598.7100.1297.7597.43100.53102.97
CCSS0.591.0894.5598.15100100.66102.49102.78
0.690.5594.1397.97101102.65103.29101.75
0.793.397.5101.13102.8103.35102.81100.5
0.895.63100.33103.41102.77101.6410097.48

0.295.8796.1394.9294.1594.9296.1395.83
0.3103.42104.06100.9298.89100.92104.06103.42
0.4103.08104.22101.899.99101.8104.22103.08
CSCS0.5102.11103.48101.55100101.55103.48102.11
0.6103.08104.23101.8100101.8104.22103.08
0.7103.42104.06100.9298.89100.92104.06103.42
0.894.9595.3194.2393.7894.2995.695.17

0.296.22103.6103.18102.26103.18103.696.22
0.396.53104.15104.36103.67104.36104.1596.53
0.495.31100.98101.85101.68101.85100.9895.31
SCSC0.594.5298.9299.9410099.9498.9394.52
0.695.31100.98101.85101.68101.85100.9895.31
0.796.53104.15104.36103.67104.36104.1596.53
0.896.23103.59103.13102.19103.13105.5896.22

0.294.9796.2294.3591.6190.591.1290.97
0.3103.71105.89102.5897.8896.5198.0298.03
0.4104.04106.17103.7699.8398.5694.1499.79
CSSS0.5103.07105.12103.2610098.8499.8999.89
0.6104.04106.17103.7699.8398.5699.7899.79
0.7103.71105.89102.5897.8996.5198.0398.03
0.894.3595.6993.9891.1790.0590.590.42

0.290.7797.7199.5799.7299.5897.790.77
0.391.1197.8399.6599.899.6597.8391.11
0.490.6796.598.598.7998.596.5190.67
SSSC0.591.959899.8310099.839891.95
0.694.82102.81103.94103.44103.94102.8194.81
0.796.72106.2106.42105.32106.42106.296.72
0.895.38104.11104.24103.18104.22104.0995.38

0.290.9791.1490.591.6194.3596.2394.99
0.398.0398.0396.5197.88102.58105.89103.71
0.495.2999.7898.5699.83103.76106.17104.04
SSCS0.599.8999.8998.84100103.26105.12103.07
0.699.8199.7998.5699.83103.76106.17104.04
0.798.0398.0396.5197.89102.59105.89103.71
0.889.9190.0789.6291.2993.5695.7494.07

0.290.9191.789.7188.6589.7191.790.91
0.391.4899.3797.595.9997.599.3791.48
0.489.6497.39100.3799.5100.3797.3989.64
SSSS0.588.6295.9399.4210099.4295.9388.62
0.689.6497.39100.3799.49100.3797.3989.64
0.791.4899.3797.5195.9997.5199.3791.48
0.890.6991.0289.1588.389.0691.2190.3

𝑎 / 𝑏 = 1 , 𝑎 / = 1 0 0 , 𝑎 / 𝑏 = 1 , 𝑐 / 𝑎 = 0 . 2 ; 𝐸 1 1 / 𝐸 2 2 = 25, 𝐺 2 3 = 0 . 2 𝐸 2 2 , 𝐺 1 3 = 𝐺 1 2 = 0 . 5 𝐸 2 2 , 𝜈 1 2 = 𝜈 2 1 = 0 . 2 5 , 𝑏 s t / = 1 , 𝑑 s t / = 2 . Each stiffener has a single lamina with fibres along its length.