Research Article

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

Table 4

Values of “ 𝑝 ” for +45/−45/+45/−45 hypar shell.

Boundary conditionsCutout size ( 𝑎 / 𝑎 )
00.10.20.30.4

CCCC00.08−1.2−7.4−16.29
CSCC01.13−6.11−21.59−29.25
CCSC00.67−5.84−21.9−28.99
CCCS00.75−5.78−21.96−29.22
CSSC0−0.82−5.14−12.44−24.09
CCSS0−0.97−5.18−12.77−24.19
CSCS00.990.531.531.52
SCSC00.930.53−0.011.87
CSSS00.770.641.36−0.29
SSSC00.740.641.34−0.07
SSCS00.580.641.35−0.3
SSSS00.440.81.660.36

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.