Results of Composite Plate (ANSYS) Laminate Stack-upDeflection - ANSYS (in)Deflection - Maple (in)Percent Error [0 90] s 5.6825.666-0.282 [0 90 0 90] s 0.71820.7146-0.50 [0 90 0 90 0 90] s 0.21410.21196 [0 90 0 90 0 90 0 90] s 0.0910.0895-1.7 [+/-30 0] s 1.4041.45853.74 [+/-45 0] s 1.2711.38228.04 [+/-60 0] s 1.4051.46283.95 [+/-30 0 +/-30 0] s 0.15920.177710.4 [+/-45 0 +/-45 0] s 0.14520.168513.81 [+/-60 0 +/-60 0] s 0.16000.179610.9 [+/-30]s6.2995.7712-9.15 [+/45]s5.7965.680-2.04 [+/-60]s6.2995.7712-9.15 [+/-30 +/-30]s0.59660.5546-7.57 [+/-45 +/-45]s0.49890.561411.13 [+/-60 +/-60]s0.59660.5546-7.57 [+/-30 +/-30 +/-30]s0.15280.171911.11 [+/-45 +/-45 +/-45]s0.13710.161114.9 [+/-60 +/-60 +/-60]s0.15280.171911.29