*** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LAMINAE STACKING LAYER NO. ORIENTATION THICKNESS MTL. TYPE 1 0.0 0.00563 1 2 45.0 0.00563 1 3 -45.0 0.00563 1 4 90.0 0.00563 1 5 90.0 0.00563 1 6 -45.0 0.00563 1 7 45.0 0.00563 1 8 0.0 0.00563 1 TOTAL THICKNESS= 0.450E-01 MATERIAL TYPE 1 ELASTIC CONSTANTS EL = 0.188E+08 ET = 0.126E+07 GLT= 0.603E+06 NULT= 0.323E+00 THERMAL COEFFICIENTS OF EXPANSION L-T COORD. TEXPL=-0.230E-06 TEXPT= 0.149E-04 MOISTURE COEFFICIENTS OF EXPANSION L-T COORD. MEXPL= 0.000E+00 MEXPT= 0.556E-02 MOISTURE VOLUME THRESHOLD, CV= 0.400E+00 Q STIFFNESS MATRIX S COMPLIANCE MATRIX 0.18932E+08 0.40985E+06 0.00000E+00 0.53191E-07 -0.17181E-07 0.00000E+00 0.40985E+06 0.12689E+07 0.00000E+00 -0.17181E-07 0.79365E-06 0.00000E+00 0.00000E+00 0.00000E+00 0.60300E+06 0.00000E+00 0.00000E+00 0.16584E-05 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LAMINATE STIFFNESS MATRIX A I B ---+--- B I D 3.594E+05 1.140E+05 -3.906E-03 I -7.324E-04 -2.708E-04 0.000E+00 1.140E+05 3.594E+05 -1.172E-02 I -2.708E-04 -1.053E-03 0.000E+00 -3.906E-03 -1.172E-02 1.227E+05 I 0.000E+00 0.000E+00 -4.044E-04 ----------------------------------+---------------------------------- -7.324E-04 -2.708E-04 0.000E+00 I 1.016E+02 1.624E+01 6.304E+00 -2.708E-04 -1.053E-03 0.000E+00 I 1.624E+01 2.596E+01 6.304E+00 0.000E+00 0.000E+00 -4.044E-04 I 6.304E+00 6.304E+00 1.771E+01 LAMINATE RESULTANT STIFFNESSES EXX= 7.177E+06 EYY= 7.177E+06 GXY= 2.724E+06 NUXY= 3.172E-01 LAMINATE COEFFICIENTS OF MUTUAL INFLUENCE NXY,X= 1.541E-09 NXY,Y= 8.541E-08 THERMAL COEFFICIENTS FOR MIDPLANE LOADS BETA-1= 4.631E-01 BETA-2= 4.631E-01 BETA-3= 1.490E-08 GAMMA-1=-1.368E-09 GAMMA-2=-1.397E-09 GAMMA-3= 0.000E+00 MOISTURE COEFFICIENTS FOR MIDPLANE LOADS PHI-1= 2.102E+02 PHI-2= 2.102E+02 PHI-3= 3.815E-06 PSI-1=-5.066E-07 PSI-2=-5.364E-07 PSI-3= 1.490E-08 COEFFICIENTS OF EXPANSION FOR LAMINATE X-Y COORD. THERMAL COEFF. MOISTURE COEFF. X-DIRECTION 9.783E-07 4.440E-04 Y-DIRECTION 9.783E-07 4.440E-04 SHEAR XY-PLANE 2.460E-13 8.763E-11 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NUMBER= 1 LAMINATE RESPONSE WITHOUT INFLUENCE OF TEMPERATURE OR MOISTURE GIVEN LAMINATE MIDPLANE LOADS NX= 1.900E+03 NY= 0.000E+00 NXY= 0.000E+00 MX= 0.000E+00 MY= 0.000E+00 MXY= 0.000E+00 CALCULATED MIDPLANE STRAINS AND CURVATURE EXO= 5.878E-03 EYO=-1.865E-03 EXYO= 9.060E-12 KX= 4.412E-08 KY=-4.169E-08 KXY=-8.646E-10 STRESS FREE TEMP.= 0.0 OPERATING TEMP.= 0.0 PERCENT MOSITURE ABSORBED= 0.000 PERCENT MOSITURE ABSORBED IS LESS THEN MOISTURE THRESHOLD THEREFORE PERCENT MOISTURE ABSORBED HAS BEEN DEFINED AS ZERO EFFECTIVE MIDPLANE LOADS DUE TO TEMP CHANGE FROM STRESS FREE TEMP TO OPERATING TEMP DELT= 0.0 NX= 0.000E+00 NY= 0.000E+00 NXY= 0.000E+00 MX= 0.000E+00 MY= 0.000E+00 MXY= 0.000E+00 EFFECTIVE MIDPLANE LOADS DUE TO A CHANGE IN MOISTURE DW= 0.000 NX= 0.000E+00 NY= 0.000E+00 NXY= 0.000E+00 MX= 0.000E+00 MY= 0.000E+00 MXY= 0.000E+00 LAMINATE RESPONSE WITH THE INFLUENCE OF TEMPERATURE AND MOISTURE MIDPLANE LOADS DUE TO CURING, MOISTURE, AND APPLIED LOAD NXBAR= 1.900E+03 NYBAR= 0.000E+00 NXYBAR= 0.000E+00 MXBAR= 0.000E+00 MYBAR= 0.000E+00 MXYBAR= 0.000E+00 MIDPLANE STRAINS & CURVATURES DUE TO CURING, MOISTURE, AND APPLIED LOAD EXO= 5.878E-03 EYO=-1.865E-03 EXYO= 9.060E-12 KX= 4.412E-08 KY=-4.169E-08 KXY=-8.646E-10 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NO.= 1 STRESS-FREE TEMP.= 0.00E+00 OPERATING TEMP.= 0.00E+00 MOIST. CONT.= 0.00E+00 MECHANICALIMID PLANE LAMINATE LOADS LOADING I NX= 1.90E+03 NY= 0.00E+00 NXY= 0.00E+00 MSW= 1 I MX= 0.00E+00 MY= 0.00E+00 MXY= 0.00E+00 IMIDPLANE LAMINATE STRAINS AND CURVATURES I EXO= 5.88E-03 EYO=-1.86E-03 EXYO= 9.06E-12 PLY I KX= 4.41E-08 KY=-4.17E-08 KXY=-8.65E-10 ANGLE PLY SIG L SIG T TAU LT SIG X SIG Y TAU XY SIGZ -------------------------------------------------------------------- 0.00E+00 1 2.72E-01 0.0 1.11E+05 4.33E+01 1.57E-05 1.11E+05 4.33E+01 1.57E-05 1.09E+00 1 2.45E+00 -------------------------------------------------------------------- 4.35E+00 2 1.10E+02 45.0 3.88E+04 3.37E+03 -4.67E+03 2.58E+04 1.64E+04 1.77E+04 4.21E+02 2 9.39E+02 -------------------------------------------------------------------- 1.66E+03 3 2.59E+03 -45.0 3.88E+04 3.37E+03 4.67E+03 2.58E+04 1.64E+04 -1.77E+04 3.73E+03 3 5.07E+03 -------------------------------------------------------------------- 6.62E+03 4 8.07E+03 90.0 -3.29E+04 6.69E+03 4.01E-04 6.69E+03 -3.29E+04 1.33E-03 9.10E+03 4 9.72E+03 -------------------------------------------------------------------- 9.92E+03 5 9.72E+03 90.0 -3.29E+04 6.69E+03 4.04E-04 6.69E+03 -3.29E+04 1.33E-03 9.10E+03 5 8.07E+03 -------------------------------------------------------------------- 6.62E+03 6 5.07E+03 -45.0 3.88E+04 3.37E+03 4.67E+03 2.58E+04 1.64E+04 -1.77E+04 3.73E+03 6 2.59E+03 -------------------------------------------------------------------- 1.66E+03 7 9.39E+02 45.0 3.88E+04 3.37E+03 -4.67E+03 2.58E+04 1.64E+04 1.77E+04 4.21E+02 7 1.10E+02 -------------------------------------------------------------------- 4.36E+00 8 2.46E+00 0.0 1.11E+05 4.33E+01 -4.81E-06 1.11E+05 4.33E+01 -4.81E-06 1.10E+00 8 2.87E-01 -------------------------------------------------------------------- 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** SYMBOL SYMBOL CORRESPONDING PRIORITY PLOTTED STRESS LOW 5 -------- X ---- STRESS IN X DIRECTION 4 -------- Y ---- STRESS IN Y DIRECTION 3 -------- S ---- SHEAR STRESS IN X-Y PLANE 2 -------- Z ---- STRESS IN Z DIRECTION HIGH 1 -------- 0 ---- ZERO LINE STRESS PLOT: LOAD CASE NO.= 1 MINIMUM STRESS= -0.25000E+05 THICKNESS THICKNESS T(I) MAXIMUM STRESS= 0.87000E+05 INCREMENT LISTED DOWN STRESS INCREMENT= 0.19667E+04 0.14075E-02 RIGHT COLUMN I MIN= -0.28000E+05 <---------STRESS--------> 0.90000E+05=MAX I PLY V V I TYPE TTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTT I !---------+---------+----0----+---------+---------+---------+---------!0.00E+00 ! ! ! 0 ! ! ! ! !1.41E-03 ! +00.0 ! ! 0 ! ! ! ! !2.82E-03 ! ! ! 0 ! ! ! ! !4.22E-03 !---------+---------+----0----+--YS---X-+---------+---------+---------!5.63E-03 ! ! ! 0 ! YS X ! ! ! !7.04E-03 ! +45.0 ! ! 0 ! YS X ! ! ! !8.45E-03 ! ! ! 0 ! YS X ! ! ! !9.85E-03 !---------+-----S---+----0Z---+--Y----X-+---------+---------+---------!1.13E-02 ! ! S ! 0Z ! Y X ! ! ! !1.27E-02 ! -45.0 ! S ! 0 Z ! Y X ! ! ! !1.41E-02 ! ! S ! 0 Z ! Y X ! ! ! !1.55E-02 !---------+---------+----0--Z-+---------+---------+---------+---------!1.69E-02 ! ! ! 0 XZ! ! ! ! !1.83E-02 ! +90.0 ! ! 0 X Z ! ! ! !1.97E-02 ! ! ! 0 X Z ! ! ! !2.11E-02 !---------+---------+----0--X-Z---------+---------+---------+---------!2.25E-02 ! ! ! 0 X Z ! ! ! !2.39E-02 ! +90.0 ! ! 0 X Z ! ! ! !2.53E-02 ! ! ! 0 XZ! ! ! ! !2.67E-02 !---------+-----S---+----0--Z-+--Y----X-+---------+---------+---------!2.82E-02 ! ! S ! 0 Z ! Y X ! ! ! !2.96E-02 ! -45.0 ! S ! 0 Z ! Y X ! ! ! !3.10E-02 ! ! S ! 0Z ! Y X ! ! ! !3.24E-02 !---------+---------+----0Z---+--YS---X-+---------+---------+---------!3.38E-02 ! ! ! 0 ! YS X ! ! ! !3.52E-02 ! +45.0 ! ! 0 ! YS X ! ! ! !3.66E-02 ! ! ! 0 ! YS X ! ! ! !3.80E-02 !---------+---------+----0----+---------+---------+---------+---------!3.94E-02 ! ! ! 0 ! ! ! ! !4.08E-02 ! +00.0 ! ! 0 ! ! ! ! !4.22E-02 ! ! ! 0 ! ! ! ! !4.36E-02 !---------+---------+----0----+---------+---------+---------+---------!4.50E-02 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NO.= 1 STRESS-FREE TEMP.= 0.00E+00 OPERATING TEMP.= 0.00E+00 MOIST. CONT.= 0.00E+00 MECHANICALIMIDPLANE LAMINATE LOADS LOADING I NX= 1.90E+03 NY= 0.00E+00 NXY= 0.00E+00 MSW= 1 I MX= 0.00E+00 MY= 0.00E+00 MXY= 0.00E+00 IMIDPLANE LAMINATE STRAINS AND CURVATURES I EXO= 5.88E-03 EYO=-1.86E-03 EXYO= 9.06E-12 PLY I KX= 4.41E-08 KY=-4.17E-08 KXY=-8.65E-10 ANGLE PLY STRN1 STRN2 STRN12 STRNX STRNY STRNXY -------------------------------------------------------------------- 1 0.0 5.88E-03 -1.86E-03 2.61E-11 5.88E-03 -1.86E-03 2.61E-11 1 -------------------------------------------------------------------- 2 45.0 2.01E-03 2.01E-03 -7.74E-03 5.88E-03 -1.86E-03 2.12E-11 2 -------------------------------------------------------------------- 3 -45.0 2.01E-03 2.01E-03 7.74E-03 5.88E-03 -1.86E-03 1.64E-11 3 -------------------------------------------------------------------- 4 90.0 -1.86E-03 5.88E-03 6.65E-10 5.88E-03 -1.86E-03 1.15E-11 4 -------------------------------------------------------------------- 5 90.0 -1.86E-03 5.88E-03 6.70E-10 5.88E-03 -1.86E-03 6.63E-12 5 -------------------------------------------------------------------- 6 -45.0 2.01E-03 2.01E-03 7.74E-03 5.88E-03 -1.86E-03 1.76E-12 6 -------------------------------------------------------------------- 7 45.0 2.01E-03 2.01E-03 -7.74E-03 5.88E-03 -1.86E-03 -3.11E-12 7 -------------------------------------------------------------------- 8 0.0 5.88E-03 -1.86E-03 -7.98E-12 5.88E-03 -1.86E-03 -7.98E-12 8 LOAD CASE NUMBER= 2 LAMINATE RESPONSE WITHOUT INFLUENCE OF TEMPERATURE OR MOISTURE GIVEN LAMINATE MIDPLANE LOADS NX= 1.900E+03 NY= 0.000E+00 NXY= 0.000E+00 MX= 0.000E+00 MY= 0.000E+00 MXY= 0.000E+00 CALCULATED MIDPLANE STRAINS AND CURVATURE EXO= 5.878E-03 EYO=-1.865E-03 EXYO= 9.060E-12 KX= 4.412E-08 KY=-4.169E-08 KXY=-8.646E-10 STRESS FREE TEMP.= 250.0 OPERATING TEMP.= 70.0 PERCENT MOSITURE ABSORBED= 0.000 PERCENT MOSITURE ABSORBED IS LESS THEN MOISTURE THRESHOLD THEREFORE PERCENT MOISTURE ABSORBED HAS BEEN DEFINED AS ZERO EFFECTIVE MIDPLANE LOADS DUE TO TEMP CHANGE FROM STRESS FREE TEMP TO OPERATING TEMP DELT=-180.0 NX=-8.336E+01 NY=-8.336E+01 NXY=-2.682E-06 MX= 2.462E-07 MY= 2.515E-07 MXY= 0.000E+00 EFFECTIVE MIDPLANE LOADS DUE TO A CHANGE IN MOISTURE DW= 0.000 NX= 0.000E+00 NY= 0.000E+00 NXY= 0.000E+00 MX= 0.000E+00 MY= 0.000E+00 MXY= 0.000E+00 LAMINATE RESPONSE WITH THE INFLUENCE OF TEMPERATURE AND MOISTURE MIDPLANE LOADS DUE TO CURING, MOISTURE, AND APPLIED LOAD NXBAR= 1.817E+03 NYBAR=-8.336E+01 NXYBAR=-2.682E-06 MXBAR= 2.462E-07 MYBAR= 2.515E-07 MXYBAR= 0.000E+00 MIDPLANE STRAINS & CURVATURES DUE TO CURING, MOISTURE, AND APPLIED LOAD EXO= 5.702E-03 EYO=-2.041E-03 EXYO=-3.522E-11 KX= 4.476E-08 KY=-4.130E-08 KXY=-1.234E-09 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NO.= 2 STRESS-FREE TEMP.= 2.50E+02 OPERATING TEMP.= 7.00E+01 MOIST. CONT.= 0.00E+00 MECHANICALIMID PLANE LAMINATE LOADS LOADING I NX= 1.90E+03 NY= 0.00E+00 NXY= 0.00E+00 MSW= 1 I MX= 0.00E+00 MY= 0.00E+00 MXY= 0.00E+00 IMIDPLANE LAMINATE STRAINS AND CURVATURES I EXO= 5.88E-03 EYO=-1.86E-03 EXYO= 9.06E-12 PLY I KX= 4.41E-08 KY=-4.17E-08 KXY=-8.65E-10 ANGLE PLY SIG L SIG T TAU LT SIG X SIG Y TAU XY SIGZ -------------------------------------------------------------------- 0.00E+00 1 1.97E+01 0.0 1.07E+05 3.13E+03 -6.57E-06 1.07E+05 3.13E+03 -6.57E-06 7.87E+01 1 1.77E+02 -------------------------------------------------------------------- 3.15E+02 2 5.75E+02 45.0 3.57E+04 6.46E+03 -4.67E+03 2.58E+04 1.64E+04 1.46E+04 1.04E+03 2 1.71E+03 -------------------------------------------------------------------- 2.59E+03 3 3.68E+03 -45.0 3.57E+04 6.46E+03 4.67E+03 2.58E+04 1.64E+04 -1.46E+04 4.97E+03 3 6.47E+03 -------------------------------------------------------------------- 8.17E+03 4 9.75E+03 90.0 -3.60E+04 9.78E+03 4.27E-04 9.78E+03 -3.60E+04 1.57E-03 1.09E+04 4 1.16E+04 -------------------------------------------------------------------- 1.18E+04 5 1.16E+04 90.0 -3.60E+04 9.78E+03 4.31E-04 9.78E+03 -3.60E+04 1.57E-03 1.09E+04 5 9.75E+03 -------------------------------------------------------------------- 8.17E+03 6 6.47E+03 -45.0 3.57E+04 6.46E+03 4.67E+03 2.58E+04 1.64E+04 -1.46E+04 4.97E+03 6 3.68E+03 -------------------------------------------------------------------- 2.59E+03 7 1.71E+03 45.0 3.57E+04 6.46E+03 -4.67E+03 2.58E+04 1.64E+04 1.46E+04 1.04E+03 7 5.75E+02 -------------------------------------------------------------------- 3.15E+02 8 1.77E+02 0.0 1.07E+05 3.13E+03 -3.59E-05 1.07E+05 3.13E+03 -3.59E-05 7.87E+01 8 1.97E+01 -------------------------------------------------------------------- 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** SYMBOL SYMBOL CORRESPONDING PRIORITY PLOTTED STRESS LOW 5 -------- X ---- STRESS IN X DIRECTION 4 -------- Y ---- STRESS IN Y DIRECTION 3 -------- S ---- SHEAR STRESS IN X-Y PLANE 2 -------- Z ---- STRESS IN Z DIRECTION HIGH 1 -------- 0 ---- ZERO LINE STRESS PLOT: LOAD CASE NO.= 2 MINIMUM STRESS= -0.25000E+05 THICKNESS THICKNESS T(I) MAXIMUM STRESS= 0.87000E+05 INCREMENT LISTED DOWN STRESS INCREMENT= 0.19667E+04 0.14075E-02 RIGHT COLUMN I MIN= -0.28000E+05 <---------STRESS--------> 0.90000E+05=MAX I PLY V V I TYPE TTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTT I !---------+---------+----0-Y--+---------+---------+---------+---------!0.00E+00 ! ! ! 0 Y ! ! ! ! !1.41E-03 ! +00.0 ! ! 0 Y ! ! ! ! !2.82E-03 ! ! ! 0 Y ! ! ! ! !4.22E-03 !---------+---------+----0----+--S----X-+---------+---------+---------!5.63E-03 ! ! ! 0 ! S X ! ! ! !7.04E-03 ! +45.0 ! ! 0Z ! S X ! ! ! !8.45E-03 ! ! ! 0Z ! S X ! ! ! !9.85E-03 !---------+------S--+----0Z---+--Y----X-+---------+---------+---------!1.13E-02 ! ! S ! 0 Z ! Y X ! ! ! !1.27E-02 ! -45.0 ! S ! 0 Z ! Y X ! ! ! !1.41E-02 ! ! S ! 0 Z ! Y X ! ! ! !1.55E-02 !---------+---------+----0---ZX---------+---------+---------+---------!1.69E-02 ! ! ! 0 Z ! ! ! !1.83E-02 ! +90.0 ! ! 0 XZ ! ! ! !1.97E-02 ! ! ! 0 XZ ! ! ! !2.11E-02 !---------+---------+----0----XZ--------+---------+---------+---------!2.25E-02 ! ! ! 0 XZ ! ! ! !2.39E-02 ! +90.0 ! ! 0 XZ ! ! ! !2.53E-02 ! ! ! 0 Z ! ! ! !2.67E-02 !---------+------S--+----0---Z+--Y----X-+---------+---------+---------!2.82E-02 ! ! S ! 0 Z ! Y X ! ! ! !2.96E-02 ! -45.0 ! S ! 0 Z ! Y X ! ! ! !3.10E-02 ! ! S ! 0 Z ! Y X ! ! ! !3.24E-02 !---------+---------+----0Z---+--S----X-+---------+---------+---------!3.38E-02 ! ! ! 0Z ! S X ! ! ! !3.52E-02 ! +45.0 ! ! 0Z ! S X ! ! ! !3.66E-02 ! ! ! 0 ! S X ! ! ! !3.80E-02 !---------+---------+----0-Y--+---------+---------+---------+---------!3.94E-02 ! ! ! 0 Y ! ! ! ! !4.08E-02 ! +00.0 ! ! 0 Y ! ! ! ! !4.22E-02 ! ! ! 0 Y ! ! ! ! !4.36E-02 !---------+---------+----0-Y--+---------+---------+---------+---------!4.50E-02 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NO.= 2 STRESS-FREE TEMP.= 2.50E+02 OPERATING TEMP.= 7.00E+01 MOIST. CONT.= 0.00E+00 MECHANICALIMIDPLANE LAMINATE LOADS LOADING I NX= 1.90E+03 NY= 0.00E+00 NXY= 0.00E+00 MSW= 1 I MX= 0.00E+00 MY= 0.00E+00 MXY= 0.00E+00 IMIDPLANE LAMINATE STRAINS AND CURVATURES I EXO= 5.88E-03 EYO=-1.86E-03 EXYO= 9.06E-12 PLY I KX= 4.41E-08 KY=-4.17E-08 KXY=-8.65E-10 ANGLE PLY STRN1 STRN2 STRN12 STRNX STRNY STRNXY -------------------------------------------------------------------- 1 0.0 5.66E-03 6.41E-04 -1.09E-11 5.66E-03 6.41E-04 -1.09E-11 1 -------------------------------------------------------------------- 2 45.0 1.79E-03 4.51E-03 -7.74E-03 7.02E-03 -7.20E-04 -2.72E-03 2 -------------------------------------------------------------------- 3 -45.0 1.79E-03 4.51E-03 7.74E-03 7.02E-03 -7.20E-04 2.72E-03 3 -------------------------------------------------------------------- 4 90.0 -2.08E-03 8.38E-03 7.09E-10 8.38E-03 -2.08E-03 2.06E-10 4 -------------------------------------------------------------------- 5 90.0 -2.08E-03 8.38E-03 7.16E-10 8.38E-03 -2.08E-03 1.99E-10 5 -------------------------------------------------------------------- 6 -45.0 1.79E-03 4.51E-03 7.74E-03 7.02E-03 -7.20E-04 2.72E-03 6 -------------------------------------------------------------------- 7 45.0 1.79E-03 4.51E-03 -7.74E-03 7.02E-03 -7.20E-04 -2.72E-03 7 -------------------------------------------------------------------- 8 0.0 5.66E-03 6.41E-04 -5.95E-11 5.66E-03 6.41E-04 -5.95E-11 8 LOAD CASE NUMBER= 3 LAMINATE RESPONSE WITHOUT INFLUENCE OF TEMPERATURE OR MOISTURE GIVEN LAMINATE MIDPLANE LOADS NX= 1.900E+03 NY= 0.000E+00 NXY= 0.000E+00 MX= 0.000E+00 MY= 0.000E+00 MXY= 0.000E+00 CALCULATED MIDPLANE STRAINS AND CURVATURE EXO= 5.878E-03 EYO=-1.865E-03 EXYO= 9.060E-12 KX= 4.412E-08 KY=-4.169E-08 KXY=-8.646E-10 STRESS FREE TEMP.= 250.0 OPERATING TEMP.= 70.0 PERCENT MOSITURE ABSORBED= 1.200 EFFECTIVE MIDPLANE LOADS DUE TO TEMP CHANGE FROM STRESS FREE TEMP TO OPERATING TEMP DELT=-180.0 NX=-8.336E+01 NY=-8.336E+01 NXY=-2.682E-06 MX= 2.462E-07 MY= 2.515E-07 MXY= 0.000E+00 EFFECTIVE MIDPLANE LOADS DUE TO A CHANGE IN MOISTURE DW=12.000 NX= 1.682E+02 NY= 1.682E+02 NXY= 3.052E-06 MX=-4.053E-07 MY=-4.292E-07 MXY= 1.192E-08 LAMINATE RESPONSE WITH THE INFLUENCE OF TEMPERATURE AND MOISTURE MIDPLANE LOADS DUE TO CURING, MOISTURE, AND APPLIED LOAD NXBAR= 1.985E+03 NYBAR= 8.480E+01 NXYBAR= 3.695E-07 MXBAR=-1.591E-07 MYBAR=-1.777E-07 MXYBAR= 1.192E-08 MIDPLANE STRAINS & CURVATURES DUE TO CURING, MOISTURE, AND APPLIED LOAD EXO= 6.057E-03 EYO=-1.685E-03 EXYO= 3.488E-11 KX= 4.394E-08 KY=-3.926E-08 KXY=-9.937E-10 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NO.= 3 STRESS-FREE TEMP.= 2.50E+02 OPERATING TEMP.= 7.00E+01 MOIST. CONT.= 1.20E+00 MECHANICALIMID PLANE LAMINATE LOADS LOADING I NX= 1.90E+03 NY= 0.00E+00 NXY= 0.00E+00 MSW= 1 I MX= 0.00E+00 MY= 0.00E+00 MXY= 0.00E+00 IMIDPLANE LAMINATE STRAINS AND CURVATURES I EXO= 5.88E-03 EYO=-1.86E-03 EXYO= 9.06E-12 PLY I KX= 4.41E-08 KY=-4.17E-08 KXY=-8.65E-10 ANGLE PLY SIG L SIG T TAU LT SIG X SIG Y TAU XY SIGZ -------------------------------------------------------------------- 0.00E+00 1 -1.20E+01 0.0 1.12E+05 -1.91E+03 3.28E-05 1.12E+05 -1.91E+03 3.28E-05 -4.81E+01 1 -1.08E+02 -------------------------------------------------------------------- -1.92E+02 2 -1.85E+02 45.0 4.08E+04 1.41E+03 -4.67E+03 2.58E+04 1.64E+04 1.97E+04 2.80E+01 2 4.47E+02 -------------------------------------------------------------------- 1.07E+03 3 1.90E+03 -45.0 4.08E+04 1.41E+03 4.67E+03 2.58E+04 1.64E+04 -1.97E+04 2.94E+03 3 4.19E+03 -------------------------------------------------------------------- 5.64E+03 4 7.00E+03 90.0 -3.09E+04 4.74E+03 3.85E-04 4.74E+03 -3.09E+04 1.17E-03 7.97E+03 4 8.55E+03 -------------------------------------------------------------------- 8.74E+03 5 8.55E+03 90.0 -3.09E+04 4.74E+03 3.89E-04 4.74E+03 -3.09E+04 1.17E-03 7.97E+03 5 7.00E+03 -------------------------------------------------------------------- 5.64E+03 6 4.19E+03 -45.0 4.08E+04 1.41E+03 4.67E+03 2.58E+04 1.64E+04 -1.97E+04 2.94E+03 6 1.90E+03 -------------------------------------------------------------------- 1.07E+03 7 4.47E+02 45.0 4.08E+04 1.41E+03 -4.67E+03 2.58E+04 1.64E+04 1.97E+04 2.80E+01 7 -1.85E+02 -------------------------------------------------------------------- -1.92E+02 8 -1.08E+02 0.0 1.12E+05 -1.91E+03 9.23E-06 1.12E+05 -1.91E+03 9.23E-06 -4.81E+01 8 -1.20E+01 -------------------------------------------------------------------- 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** SYMBOL SYMBOL CORRESPONDING PRIORITY PLOTTED STRESS LOW 5 -------- X ---- STRESS IN X DIRECTION 4 -------- Y ---- STRESS IN Y DIRECTION 3 -------- S ---- SHEAR STRESS IN X-Y PLANE 2 -------- Z ---- STRESS IN Z DIRECTION HIGH 1 -------- 0 ---- ZERO LINE STRESS PLOT: LOAD CASE NO.= 3 MINIMUM STRESS= -0.25000E+05 THICKNESS THICKNESS T(I) MAXIMUM STRESS= 0.87000E+05 INCREMENT LISTED DOWN STRESS INCREMENT= 0.19667E+04 0.14075E-02 RIGHT COLUMN I MIN= -0.28000E+05 <---------STRESS--------> 0.90000E+05=MAX I PLY V V I TYPE TTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTTT I !---------+---------+---Y0----+---------+---------+---------+---------!0.00E+00 ! ! ! Y0 ! ! ! ! !1.41E-03 ! +00.0 ! ! Y0 ! ! ! ! !2.82E-03 ! ! ! Y0 ! ! ! ! !4.22E-03 !---------+---------+----0----+--Y-S--X-+---------+---------+---------!5.63E-03 ! ! ! 0 ! Y S X ! ! ! !7.04E-03 ! +45.0 ! ! 0 ! Y S X ! ! ! !8.45E-03 ! ! ! 0 ! Y S X ! ! ! !9.85E-03 !---------+----S----+----0Z---+--Y----X-+---------+---------+---------!1.13E-02 ! ! S ! 0Z ! Y X ! ! ! !1.27E-02 ! -45.0 ! S ! 0Z ! Y X ! ! ! !1.41E-02 ! ! S ! 0 Z ! Y X ! ! ! !1.55E-02 !---------+---------+----0-XZ-+---------+---------+---------+---------!1.69E-02 ! ! ! 0 X Z! ! ! ! !1.83E-02 ! +90.0 ! ! 0 X Z! ! ! ! !1.97E-02 ! ! ! 0 X Z! ! ! ! !2.11E-02 !---------+---------+----0-X-Z+---------+---------+---------+---------!2.25E-02 ! ! ! 0 X Z! ! ! ! !2.39E-02 ! +90.0 ! ! 0 X Z! ! ! ! !2.53E-02 ! ! ! 0 X Z! ! ! ! !2.67E-02 !---------+----S----+----0--Z-+--Y----X-+---------+---------+---------!2.82E-02 ! ! S ! 0 Z ! Y X ! ! ! !2.96E-02 ! -45.0 ! S ! 0Z ! Y X ! ! ! !3.10E-02 ! ! S ! 0Z ! Y X ! ! ! !3.24E-02 !---------+---------+----0Z---+--Y-S--X-+---------+---------+---------!3.38E-02 ! ! ! 0 ! Y S X ! ! ! !3.52E-02 ! +45.0 ! ! 0 ! Y S X ! ! ! !3.66E-02 ! ! ! 0 ! Y S X ! ! ! !3.80E-02 !---------+---------+---Y0----+---------+---------+---------+---------!3.94E-02 ! ! ! Y0 ! ! ! ! !4.08E-02 ! +00.0 ! ! Y0 ! ! ! ! !4.22E-02 ! ! ! Y0 ! ! ! ! !4.36E-02 !---------+---------+---Y0----+---------+---------+---------+---------!4.50E-02 1 *** ASTM-STP775 T300/5208 GR/EP LAMINATE: LOADS AND STRESS FOR [0/45/-45/90]S ** LOAD CASE NO.= 3 STRESS-FREE TEMP.= 2.50E+02 OPERATING TEMP.= 7.00E+01 MOIST. CONT.= 1.20E+00 MECHANICALIMIDPLANE LAMINATE LOADS LOADING I NX= 1.90E+03 NY= 0.00E+00 NXY= 0.00E+00 MSW= 1 I MX= 0.00E+00 MY= 0.00E+00 MXY= 0.00E+00 IMIDPLANE LAMINATE STRAINS AND CURVATURES I EXO= 5.88E-03 EYO=-1.86E-03 EXYO= 9.06E-12 PLY I KX= 4.41E-08 KY=-4.17E-08 KXY=-8.65E-10 ANGLE PLY STRN1 STRN2 STRN12 STRNX STRNY STRNXY -------------------------------------------------------------------- 1 0.0 6.02E-03 -3.45E-03 5.45E-11 6.02E-03 -3.45E-03 5.45E-11 1 -------------------------------------------------------------------- 2 45.0 2.14E-03 4.20E-04 -7.74E-03 5.15E-03 -2.59E-03 1.72E-03 2 -------------------------------------------------------------------- 3 -45.0 2.14E-03 4.20E-04 7.74E-03 5.15E-03 -2.59E-03 -1.72E-03 3 -------------------------------------------------------------------- 4 90.0 -1.73E-03 4.29E-03 6.39E-10 4.29E-03 -1.73E-03 -1.13E-10 4 -------------------------------------------------------------------- 5 90.0 -1.73E-03 4.29E-03 6.45E-10 4.29E-03 -1.73E-03 -1.19E-10 5 -------------------------------------------------------------------- 6 -45.0 2.14E-03 4.20E-04 7.74E-03 5.15E-03 -2.59E-03 -1.72E-03 6 -------------------------------------------------------------------- 7 45.0 2.14E-03 4.20E-04 -7.74E-03 5.15E-03 -2.59E-03 1.72E-03 7 -------------------------------------------------------------------- 8 0.0 6.02E-03 -3.45E-03 1.53E-11 6.02E-03 -3.45E-03 1.53E-11 8