Front Wing Assembly

Weight: 48.4693 lbm Notes: The lengths of the wings is mostly arbitrary and can be changed based upon final dimensions and weight requirements. The material used is CFRP, Epoxy Matrix. The gap in the center was chosen as 15” based upon the car’s frame, but can easily be modified based upon the actual values once the shell and nosecone are added. There are three holes on each of the center mounting panels so that they can be mounted to the shell. The clearance between the center mounting panels and the central airfoil is basically non-existent and if necessary the center mounting panels can be trimmed. The center, left, and right mounting panels have some excess on the bottom that can be trimmed if necessary, although they were the basis of most dimensioning so the software might freak out a bit. All fasteners are Mil. Spec. 18-8 Stainless Steel Phillips Flat Head Screws downloaded off of McMaster, screw clearance holes use close fit: https://www.mcmaster.com/#96877a635/=1aimemv