Hi, can you help me with some questions, I am struggling on how to calculating cg margins on an aircraft?
@mostafadjamali7185 жыл бұрын
how to find the aerodynamic center of the wing experimentally ?
@ItsNotAllRainbows_and_Unicorns3 жыл бұрын
Usually it's a quarter chord length from the leading edge of the airfoil. In addition the aerodynamic center does not change with variation in angle of attack.
@arnavkumar30602 жыл бұрын
What is the right hand rule the prof. is mentioning ?
@dondocentone13345 ай бұрын
The moment causing the aircraft to pitch down has negative sign and vice versa. It is in agreement with general right hand rule for moments f.e. in static analysis of cantilever beam (clockwise rotation has a negative sign...).
@dondocentone13345 ай бұрын
And maybe prof. probably recalls the right hand rule of gyroscopic effect for propeller