I am sizing a panel in HyperSizer. This panel is a sandwich structure, contains a honeycomb core and carbon fiber laminate face sheets. Because of a “pillowing” effect of composite skins in the honeycomb cells during curing, the strength of the skin is typically lower than a monolithic laminates. Therefore a correction factor will be applied for strength of the face sheets/skin materials in a honeycomb structure, while calculating MOS for the ply strength. Does HyperSizer already include this knockdown factor while calculating MOS in the failure tab?