Research Article

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

Table 7

Values of “ 𝑟 ” for 0/90/0/90 hypar shells.

Edge condition 𝑦 𝑥
0.20.30.40.50.60.70.8

CCCC0.297.5298.1999.1499.6999.1298.1797.49
0.398.2398.8399.5199.8799.5198.8198.22
0.499.2599.6199.8699.9699.8699.699.23
0.599.86100.03100.03100100.03100.0399.86
0.699.2399.699.8699.9799.8699.6199.25
0.798.2298.8199.5199.8699.5198.8398.23
0.897.4998.1699.0999.6899.198.1697.51

CSCC0.299.5399.69100.03100.24100.0399.6899.47
0.3100.24100.15100.25100.35100.26100.16100.21
0.4100.0999.84100100.19100.0299.86100.1
0.597.9498.6299.3310099.3498.6398.79
0.697.3497.1598.399.7898.2997.1697.35
0.796.3795.9996.9899.4296.989696.38
0.895.8795.2995.6996.6895.795.395.89

CCSC0.296.2196.7797.7599.07100.12100.1399.48
0.395.5796.3597.5198.8399.83100.0999.72
0.495.6697.1798.5299.4299.96100.24100.13
0.595.9599.5999.9100100.13100.35100.38
0.695.5897.0898.4699.3999.96100.24100.13
0.795.5296.397.4698.899.83100.199.72
0.896.2196.7597.6898.99100.1100.1299.49

CCCS0.295.8995.3195.7196.6495.6795.2995.87
0.396.389696.9799.4196.9695.9996.37
0.497.3597.1698.2999.7898.2997.1597.34
0.598.7998.6399.3410099.3398.6298.78
0.6100.199.86100.02100.1910099.84100.08
0.7100.21100.16100.26100.35100.25100.15100.21
0.899.3299.4999.83100.0599.8399.4799.31

CSSC0.298.7998.8299.299.86100.55100.89100.79
0.398.9599.2799.66100.08100.48100.8100.95
0.498.27100.33100.3100.38100.43100.46100.57
0.596.2597.5998.9100100.3299.9399.75
0.696.0996.397.2999.15100.2299.499.01
0.796.6296.1996.6798.31100.1798.9598.66
0.897.5796.8396.7297.2398.5698.6198.7

CCSS0.297.5496.896.7397.2498.5198.5698.64
0.396.6196.1896.6698.3100.1398.9198.62
0.496.1496.3497.3299.15100.299.3798.99
0.596.3297.6998.95100100.2999.999.73
0.698.28100.3100.27100.34100.38100.41100.53
0.798.8499.1999.6100.03100.44100.76100.91
0.898.6598.6798.9299.56100.32100.69100.63

CSCS0.286.5386.5186.9586.1686.9786.4986.48
0.392.992.7792.8492.8792.8492.7592.84
0.496.5296.497.1797.797.1796.3896.47
0.597.1797.4198.8510098.8497.4197.17
0.696.4796.3997.1797.797.1796.496.5
0.792.8492.7592.8492.8892.8492.7792.9
0.886.1786.1886.6687.0286.7386.3386.33

SCSC0.286.3892.8997.1498.2597.1292.8786.36
0.386.4392.9296.9798.2396.9392.8785.96
0.486.992.9297.4599.2597.3992.8786.84
0.587.1392.8597.7110097.7192.8587.13
0.686.8492.8797.3999.2597.4592.9286.9
0.786.3992.8796.9398.2296.9592.9286.43
0.886.2792.7697.0998.1497.0592.886.31

CSSS0.287.5587.487.5788.0388.7389.1488.85
0.394.3794.4494.0694.0195.1896.6596.62
0.498.8598.8498.3398.3399.99101.94101.87
0.5100.37100.2899.82100101.89103.9103.68
0.698.7698.7798.2998.3199.99101.94101.87
0.794.2894.3794.0293.9895.1696.6396.59
0.887.1787.187.2987.7488.488.8588.6

SSSC0.289.0196.86102.03103.78102.0396.8688.99
0.389.296.84102.06103.95102.0696.8289.16
0.488.795.26100.02101.88100.0395.2688.7
0.587.9494.0298.3210098.3994.188
0.687.4794.0798.3699.8898.4494.1887.55
0.787.2994.4798.9100.498.9894.5687.38
0.887.3494.2698.78100.3398.8494.3587.42

SSCS0.288.8389.0988.688887.5387.3487.45
0.396.5896.6295.1593.9794.0194.3794.27
0.4101.85101.9499.9898.398.2798.7798.78
0.5103.67103.9101.8910099.82100.28100.36
0.6101.87101.9499.9898.3398.3298.8398.83
0.796.6196.6595.179494.0594.4494.37
0.888.4388.788.3387.7787.2687.2187.22

SSSS0.283.7986.9687.8588.0687.9387.0683.88
0.387.2493.0494.6194.7594.793.1287.28
0.488.294.8998.0998.7898.294.9488.2
0.588.3895.0899.0910099.0995.0888.38
0.688.2194.9598.298.7898.0994.8988.2
0.787.2893.1294.6894.7594.6193.0487.24
0.883.7286.987.6587.7687.4486.7983.43

𝑎 / 𝑏 = 1 , 𝑎 / = 1 0 0 , 𝑎 / 𝑏 = 1 , 𝑐 / 𝑎 = 0 . 2 ; 𝐸 1 1 / 𝐸 2 2 = 2 5 , 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.