Re: [RCSE] Initial CG on a scratch ship...

2006-04-20 Thread Frank Deichsel
Title: Initial CG on a scratch ship...



That is a good start for the CG, but the other part 
of the equation is the horizontal stab. How big is the tail, how far from the 
wing is it it and what is the decalage? Here's something worthwhile reading: http://www.fatlion.com/sailplanes/decalage.html
 
Is this a scale ship??
 
 
Frank
 
 
 

  - Original Message - 
  From: 
  George Voss 
  
  To: 'Douglas, Brent' ; soaring@airage.com 
  Sent: Thursday, April 20, 2006 12:20 
  PM
  Subject: RE: [RCSE] Initial CG on a 
  scratch ship...
  
  
  You need to find the 
  MAC or Mean Aerodynamic Chord, which is the average chord.  Assuming a 
  straight leading edge and a tapered TE, if it’s a straight taper , measure the 
  root, add the tip and divide by 2.  That is the average chord.  So, 
  make a mark 8” back from the LE and that’s the average chord.  30% of 
   8 is 2.4, just like you calculated.  I’d start there.  
  
   
  If the TE has more 
  than one taper, you will need to take into that into account.  
  
   
  George 
  Voss
  
  
  
  
  From: 
  Douglas, Brent [mailto:[EMAIL PROTECTED] Sent: Thursday, April 20, 2006 12:39 
  PMTo: 
  soaring@airage.comSubject: 
  [RCSE] Initial CG on a scratch ship...
   
  Just trying to get a rough idea 
  where to start here, what formula you might use to come up with a starting 
  CG…. Picture a 200 inch wing, root chord about 11 inches, tip about 5, 
  straight leading edge, tapering TE.
  Modern airfoil, HQ 2.5, 12 - 10 
  percent thick.    My thought was to go mid span, take some 
  percentage of the chord there, then mark the root that far back - 
  example:  30% of 8" becomes 2.4 inches - mark the root at 2.4 inches from 
  the leading edge.  
  2 
  questions - how far off is that logic, how far off is 
  30%?  
  I'm towing this ship for the first 
  flight, so I'd like to be pretty close, erring to the nose heavy 
  side. 
  Thanks!Brent 
  
   


Re: [RCSE] Initial CG on a scratch ship...

2006-04-20 Thread Harley Michaelis
Title: Initial CG on a scratch ship...



Brent. . .I would never tow a ship on its first 
flight. Can't you find a little hill or mound and start with some hand 
tosses? 
 
Having quite frequently seen inquiries about an 
initial CG, it might be of value to follow the steps I do with a new ship to 
avoid calamity. All of mine are scratch built and each is a 
little different, so it has to be sorted out for each one, step by 
step. 
 
Just go to the Genie pages at http://genie.rchomepage.com/ and get 
into File 8.

  - Original Message - 
  From: 
  Douglas, Brent 
  
  To: soaring@airage.com 
  Sent: Thursday, April 20, 2006 10:39 
  AM
  Subject: [RCSE] Initial CG on a scratch 
  ship...
  
  Just trying to get a rough idea where to start 
  here, what formula you might use to come up with a starting CG…. Picture a 200 
  inch wing, root chord about 11 inches, tip about 5, straight leading edge, 
  tapering TE.
  Modern airfoil, HQ 2.5, 12 - 10 percent 
  thick.    My thought was to go mid span, take some percentage 
  of the chord there, then mark the root that far back - example:  30% of 
  8" becomes 2.4 inches - mark the root at 2.4 inches from the leading 
  edge.  
  2 questions - how far off is that logic, how far 
  off is 30%?  
  I'm towing this ship for the first flight, so I'd 
  like to be pretty close, erring to the nose heavy side. 
  Thanks!Brent 



Re: [RCSE] Initial CG on a scratch ship...

2006-04-20 Thread Bill Swingle

Your logic sounds quite reasonable for your planform.

Bill Swingle
Janesville, CA


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RE: [RCSE] Initial CG on a scratch ship...

2006-04-20 Thread George Voss
Title: Initial CG on a scratch ship...








You need to find the MAC or Mean
Aerodynamic Chord, which is the average chord.  Assuming a straight leading
edge and a tapered TE, if it’s a straight taper , measure the root, add
the tip and divide by 2.  That is the average chord.  So, make a mark
8” back from the LE and that’s the average chord.  30% of  8
is 2.4, just like you calculated.  I’d start there.  

 

If the TE has more than one taper, you
will need to take into that into account.  

 

George Voss









From: Douglas, Brent
[mailto:[EMAIL PROTECTED] 
Sent: Thursday, April 20, 2006
12:39 PM
To: soaring@airage.com
Subject: [RCSE] Initial CG on a
scratch ship...



 

Just
trying to get a rough idea where to start here, what formula you might use to
come up with a starting CG…. Picture a 200 inch wing, root chord about 11
inches, tip about 5, straight leading edge, tapering TE.

Modern
airfoil, HQ 2.5, 12 - 10 percent thick.    My thought was to go
mid span, take some percentage of the chord there, then mark the root that far
back - example:  30% of 8" becomes 2.4 inches - mark the root at 2.4
inches from the leading edge.  

2
questions - how far off is that logic, how far off is
30%?  

I'm
towing this ship for the first flight, so I'd like to be pretty close, erring
to the nose heavy side. 

Thanks!
Brent