Web-Based Composite Analysis Tools

3pcsolver001 performs strength analysis of composite laminates subjected to static forces and moments, uniform temperature  and moisture effects. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver002 performs bending  analyses of simply supported fully anisotropic laminate composite plates subjected to the transverse loads: (i) Uniformly Distributed Pressure Load (ii) Sinusoidal Pressure Load (iii) Partial Pressure Load, and (iv) Point Load. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver003 performs buckling analyses of simply supported fully anisotropic laminate composite plates subjected to various combination of edge compression/tension and/or shear loads. The analysis is applicable to a wide variety of ply/lamina materials and laminates 

3pcsolver004 performs free Vibration analyses of simply supported fully anisotropic laminate composite plates. The effects of edge compression/tension and/or shear loads on the natural frequencies of laminates can also be included. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver005 performs stress analysis of sandwich panels subjected to static forces and moments per unit length, uniform temperature and moisture variations. Furthermore, it performs checks for

all failure modes such as strength failure of face sheets and core, shear crimping, wrinkling, Intracellular buckling/dimpling, core crush and face sheet disbond  

3pcsolver006 performs bending  analyses of simply supported sandwich plates subjected to the transverse loads: (i) Uniformly Distributed Pressure Load (ii) Sinusoidal Pressure Load (iii) Partial Pressure Load, and (iv) Point Load. The analysis is applicable to a wide variety of ply/lamina and core materials, and sandwich plates

3pcsolver007 performs buckling analyses of simply supported sandwich plates subjected to various combination of edge compression/tension and/or shear loads. The analysis is applicable to a wide variety of ply/lamina and core materials, and sandwich plates 

3pcsolver008 performs free Vibration analyses of simply supported sandwich plates. The effects of edge compression/tension and/or shear loads on the natural frequencies of sandwich plates can be included. The analysis is applicable to  a wide variety of ply/lamina and core materials, and sandwich plates

3pcsolver009 performs stress concentration  analyses of laminated composite plates having circular and elliptical holes (or cutouts). Furthermore, it predicts notched strength of laminated composite plates based on standard composite failure criteria. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver010 performs stress concentration  analyses of Sandwich composite plates having circular and elliptical holes (or cutouts). Furthermore, it predicts notched strength of laminated composite face sheets based on standard composite failure criteria. The analysis is applicable to  a wide variety of ply/lamina and core materials, and sandwich plates

3pcsolver011 performs strength analysis of laminated composite cylindrical panels and shells subjected to static forces and moments, uniform temperature  and moisture effects. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver012 performs bending  analyses of simply supported fully anisotropic laminate composite cylindrical panels and shells subjected to the transverse loads: (i) Uniformly Distributed Pressure Load (ii) Sinusoidal Pressure Load (iii) Partial Pressure Load, and (iv) Point Load. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver013 performs buckling analyses of simply supported fully anisotropic laminate composite cylindrical panels and shells subjected subjected to various combination of edge compression/tension and/or shear loads. The analysis is applicable to a wide variety of ply/lamina materials and laminates 

3pcsolver014 performs free Vibration analyses of simply supported fully anisotropic laminate composite cylindrical panels and shells including the effects of edge compression/tension and/or shear loads. The analysis is applicable to a wide variety of ply/lamina materials and laminates

3pcsolver015 performs stress analysis of cylindrical sandwich panels and shells subjected to static forces and moments per unit length, uniform temperature and moisture variations. Furthermore, it performs checks for all failure modes such as strength failure of face sheets and core, shear crimping, wrinkling, Intracellular buckling/dimpling, core crush etc.

3pcsolver016 performs bending  analyses of simply supported cylindrical sandwich panels and shells subjected to the transverse loads: (i) Uniformly Distributed Pressure Load (ii) Sinusoidal Pressure Load (iii) Partial Pressure Load, and (iv) Point Load. The analysis is applicable to a wide variety of ply/lamina and core materials, and sandwich panels

3pcsolver017 performs buckling analyses of simply supported cylindrical sandwich panels and shells subjected subjected to various combination of edge compression/tension and/or shear loads. The analysis is applicable to a wide variety of ply/lamina and core materials, and sandwich panels 

3pcsolver014 performs free Vibration analyses of simply supported  cylindrical sandwich panels and shells including the effects of edge compression/tension and/or shear loads. The analysis is applicable to a wide variety of ply/lamina and core materials, and sandwich panels