Andy_RR
Well-Known Member
Does anyone have to hand any papers, NACA reports etc that describe or illustrate how to calculate/derive CD/CL data for a symmetrical but hinged airfoil section - i.e empennage.
Not looking to be too fancy, but researching a aerodynamic/kinematic model for an autopilot pitch controller.
Cheers,
Andy
Not looking to be too fancy, but researching a aerodynamic/kinematic model for an autopilot pitch controller.
Cheers,
Andy