[NSRCA-discussion] Wt. & Bal.

[Nat Penton]

Bob
The following equation will work with fuselage level 

Lm = [ Lt ( W - Wm ) ] / W
             
     Lm   distance from mains to CG
     Lt     distance from mains to tailwheel
     W     weight of airplane, any units
     Wm  weight on mains
                                                           Nat
  ----- Original Message ----- 
  From: Bob Miller 
  To: NSRCA Mailing List 
  Sent: Monday, May 28, 2007 10:50 AM
  Subject: [NSRCA-discussion] Wt. & Bal.


  I think I saw a spread sheet some time ago that was set up to determine CG using scales as in full size aircraft.  Anybody ?

  Bob M.


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