Abstract: A method and system for making and forming turbine blades. The method and system can include steps for determining stress loads on amore turbine blades; constructing one or more molds for components of the turbine blade in which a turbine-forming substance is injected; applying a resin to an interior portion of the one or more molds; forming one or more partitions within the one or more molds; coupling the one or more molds; injecting the blade-forming substance into the coupled one or more molds; regulating the pressure in the coupled one or more molds; voiding any excess air or resin in the coupled one or more molds; and allowing the blade-forming substance injected into the coupled one or more molds to harden.