Build the Hybrid Aeros

The next section covers the addition of a forward set of canards onto the projectile's nose and the process of determining and verifying the hybrid spin/fin aerodynamic coefficients for the final round configuration. Since the user has already determined the aerodynamics of the spin-stabilized projectile alone, they should now proceed to Aero Direct Input to lock in the appropriate spin-stabilized aerodynamic data before adding the canards.

The basic steps for this section are as follows:

Lock/save basic aeros
- Lock Magnus and Magnus Diriv tables
- Lock specific columns of the basic aeros table
- Save a copy of the projectile with the locked aeros for pasting back into the hybrid model
- Unlock the basic aeros columns
Build up the forward canards
Generate the Finner aeros
Paste the spinner column results back into appropriate Finner Body aeros columns
Run Contraj to create the combine basic aeros table and paste and lock the result into the basic aeros table
Create and lock the Forebody Aeros table