Next either copy the basic Aero tables to excel or some other tabular data sheet or lock the following columns in the "Basic Aeros" Table. For this tutorial we will lock the aeros and save a copy of the projectile file before adding the forward canards. We will return to this saved projectile to copy the locked column back into our working model.

• CX0 – Zero Yaw Axial Drag
• CNa – Normal Force Derivative (sin α)
• CMQ – Pitch Damping
• Clp – Roll Damping
• CPN- Center of Pressure (Calibers from nose)

Previous  Top  Next

© 2025 Arrow Tech Associates