RA Cores Custom wing quote work sheet

In order to properly fill your custom glider or pattern wing order, we need the following information:

Layout of airfoil parts relative to chord

Layout of wing parts relative to span

Airfoil 1 or chord in inches
Airfoil 2 or chord in inches

Panel length from Airfoil 1 to Airfoil 2
Panel taper (i.e. straight trailing edge or tip leading edge is 1.5" behind root leading edge)

Airfoil 3 or chord in inches

Panel length from Airfoil 2 to Airfoil 3
Panel taper (i.e. straight trailing edge or tip leading edge is 1.5" behind root leading edge)

Airfoil 4 or chord in inches

Panel length from Airfoil 3 to Airfoil 4
Panel taper (i.e. straight trailing edge or tip leading edge is 1.5" behind root leading edge)

Wing sheeting thickness or
Leading edge allowance or
Trailing edge allowance or

Washout (in degrees or raise tip trailing edge 1/4") or

Additional questions or instructions

Email address for quote results or further questions

This form can also be printed from your browser and faxed or snail mailed to us

RA Cores
P.O. Box 863
Southbridge, MA 01550

Internet: racores@world.std.com or info@racores.com
or visit our home page at http://www.racores.com/index.html
Voice or Fax: (508) 765-9998