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

Table 8: Comparison of normalized central moments, $M_{1}^{*}$ , of [0/90/0] saddle-shaped panels, with SS1 and SS4 boundary constraints, under uniform load.

Normalized Central Moment, *, $M_{1}^{}$ 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	108.15821	100.407 (7.167)^*	108.15821	100.407 (7.167)^*
10	123.00260	106.654 (13.291)^*	123.00260	106.654 (13.291)^*
20	128.14462	89.143 (30.436)^*	128.14462	89.143 (30.436)^*
50	129.84572	37.110 (71.4199)^*	129.84572	37.110 (71.420)^*
100	130.733356	11.488 (91.213)^*	130.733356	11.488 (91.213)^*

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