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 (choose from Selig's database) ______________ chord in inches _________
Airfoil 2 (choose from Selig's database) ______________ 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 (choose from Selig's database) ______________ 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 (choose from Selig's database) ______________ 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 ______________
Leading edge allowance ______________
Trailing edge allowance ______________

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

Additional questions or instructions









Comments/questions









Email address for quote results or postal address





This form can 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