kral27
May 08, 2006, 12:38 AM
Where would be a good starting point for a safe first flight CG location. The tail has not yet been designed yet. Here is a image of my design; the shaded area represents the suspected CG region.
Since the image did not upload to scale the dimensions are as follows:
*Center Panel: 7.6x23cm
*Inboard Panels: 381x254mm (7.6deg swept)
*Outboard Panels 381x254mm (11.4deg swept-from center panel; 3.8deg from inboard panels)
*Tip Panels: 190x254mm {(19deg swept from center panel) 9cm tip chord en 254mm root chord} *** Tip Panels will be at 45 deg angle from center panel...
airfoil is NACA 6409 (constant chord swept wing)
Since the image did not upload to scale the dimensions are as follows:
*Center Panel: 7.6x23cm
*Inboard Panels: 381x254mm (7.6deg swept)
*Outboard Panels 381x254mm (11.4deg swept-from center panel; 3.8deg from inboard panels)
*Tip Panels: 190x254mm {(19deg swept from center panel) 9cm tip chord en 254mm root chord} *** Tip Panels will be at 45 deg angle from center panel...
airfoil is NACA 6409 (constant chord swept wing)