CG Calculator for Delta Wings PDF Print E-mail
Written by Administrator   
Monday, 14 February 2011 14:25

Simple calculator for determining The CG distance from the Leading edge at the root chords when the percent MAC is known.

Enter Root Chord (A):
Enter Tip Chord (b):
Enter Sweep Distance (S):
Enter Half Span (Y):
Enter %MAC balance Point:
Sweep Distance @ MAC (C) =
Mean Aerodynamic Chord (MAC) =
MAC Distance from Root (d) =
balance Point @ Root Chord (CG)=

Note:
A 25% of MAC is generally accepted as a good starting point for the CG of a conventional tailed aircraft. The normal range most often falls between 25-30% of MAC

Use this calculator to determine percent of MAC for a given CG

Enter Root Cord (A):
Enter Tip Cord (b):
Enter Sweep Distance (S):
Enter Half Span (Y):
Enter Center of Gravity (CG):
Sweep Distance @ MAC (C) =
Mean Aerodynamic Cord (MAC) =
MAC Distance from Root (d) =
% Mean Aerodynamic Cord (%MAC) =

Last Updated on Monday, 14 February 2011 14:36
 
Copyright © 2014 White Hills Radio Flyers. All Rights Reserved.
Joomla! is Free Software released under the GNU/GPL License.