Enter values for Wing and Tail then calculate to solve for their Aerodynamic Center and surface area. Note, these values are for half of the aircraft's wing.

Aircraft Center of Gravity (CG)

L:
*L is the distance between the AC of the tail and wing.

Canard Configuration

AUW (optional):
oz
grams

Power in Watts (optional):

CG (P) distance from AC:

CG from Leading Edge:

Total Surface Area:

Wing Loading: *

Power to Weight:

* Wing Loading calculation assumes wing measurments were provided in either cm or inches.