Comparison of normalized central deflections, , of [0/90/0] saddle-shaped panels, with SS1 and SS4 boundary constraints, under uniform load.

Table 6: Comparison of normalized central deflections, $u_{3}^{*}$ , of [0/90/0] saddle-shaped panels, with SS1 and SS4 boundary constraints, under uniform load.

Normalized Central Deflection, $u_{3}^{}$ , of [0/90/0] Saddle-Shaped Panels under Uniform Load*
a/h	R₁/a = -10, R₂/a = 10 (SS1) [96,98]	R₁/a = -10, R₂/a = 10 (SS4) [97]	R₁/a = 10, R₂/a = -10 (SS1) [96,98]	R₁/a = 10, R₂/a = -10 (SS4) [97]
5	21.86863	20.279 (7.269)^*	21.86863	20.279 (7.269)^*
10	10.90079	9.433 (13.465)^*	10.90079	9.433 (13.465⁾^*
20	7.76184	5.366 (30.867)^*	7.76184	5.366 (30.866)^*
50	6.84781	1.887 (72.444)^*	6.84781	1.887 (72.444)^*
100	6.73717	0.504 (92.519)^*	6.73717	0.504 (92.519)^*

% difference between SS1 and SS4 = $|\frac{S S 1 - S S 4}{S S 1}| 100.$