This screen is used to determine the drag coefficient for a fuselage. You must enter;
1. Fuselage length
2. Maximum Fuselage Diameter
The units are the units selected in the Drag Breakdown Tab
After the above dimensions are entered the drag coefficient will be derived. if the Ok button is pressed then the derived drag coefficient will be returned to the Edit Drag Breakdown Item screen. If the Cancel button is pressed then the Edit Drag Breakdown Item screen will remain unchanged.