I need a CAD Aerofoil turbine blade component designed in SolidWorks ASAP

Design details: Hi there,

I need a CAD Aerofoil turbine blade component designed in SolidWorks.

The task is to construct SolidWorks geometric models of a turbine blade that consists of a standard NACA aerofoil blade profile attached to a triangular blade root. The root of each blade must fit into a recessed triangular pocket in an existing rotor hub assembly 132.0 mm in diameter, as shown in attached file, and fixed in place with two M4 cap head screws. The length of each blade (the span length from root to tip) is 33.0 mm and the width of each blade (the chord length from leading edge to trailing edge) is 34.0 mm. The exact design of the triangular blade root should be chosen by the designer, but must be 3.125 mm thick to fit flush in the recessed pocket in the rotor hub. The turbine blade does not need to be centred over the thickness of the rotor hub. When fitted to the rotor, all the turbine blades must fit into a 200.0 mm diameter housing with a tip clearance of 1.0 mm, which means that the outer edge of each blade must also be curved with a radius of 99.0 mm. The inner edge of the aerofoil section, where it mates with the triangular blade root, must also be curved, with a radius of 66.0 mm. The three corners of the triangular root should be filleted with a radius of 2.5 mm.

Please take a look at the extra notes, as these show the exact procedure to follow. It is pretty self explanatory and should be relatively simple for the right designer to follow.

Will be looking for further work in the future and looking to strike up a good working relationship with the right designer.

Thanks