Thanks for your reply.

I attached my subroutine for nodal stress projecting as well as the one in the shell3d elmt of Feap. ( should I attach my complete element subroutine? )
I also put some pictures to show the boundary problem and stress result.
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here is the result of stress, node, 1, numnp:
feap * * LINEar-ELAStic.....3D.....QUADrilateral-ELEMent
N o d a l P r o j e c t i o n s
Node 1-Pr.Value 2-Pr.Value 3-Pr.Value 1-Pr.Angle
I_1 Value J_2 Value J_3 Value
1 Value 2 Value 3 Value
1 2.3129E+02 5.5310E+01 3.6246E+01 0.0000E+00
1.0762E+02 1.8625E+02 3.2012E+05
2.3129E+02 5.5310E+01 3.6246E+01
as well as node 17:
N o d a l P r o j e c t i o n s
Node 1-Pr.Value 2-Pr.Value 3-Pr.Value 1-Pr.Angle
I_1 Value J_2 Value J_3 Value
1 Value 2 Value 3 Value
17 2.0024E+02 4.6883E+01 -3.4369E+00 0.0000E+00
8.1230E+01 1.8376E+02 2.3997E+05
2.0024E+02 4.6883E+01 -3.4369E+00
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Due to plane stress model, sig_33=0 and my order in sigma plotting is:
xx-stress yy-stress xy-stress xx-moment yy-moment xy-moment ...
Thank you for your attention.