Calculating Load on primary control surfaces for suitable actuator selection
Calculating Load on primary control surfaces for suitable actuator selection
(OP)
Hi Guys,
The question is pretty much in the topic.
I need to select some actuators for the ailerons and ruddervator on a project I'm working on. The actuators need to be able to operate during the aircrafts most testing flight conditions.
So how do I determine what load will be experienced by the actuator (control surface)?
Thanks
The question is pretty much in the topic.
I need to select some actuators for the ailerons and ruddervator on a project I'm working on. The actuators need to be able to operate during the aircrafts most testing flight conditions.
So how do I determine what load will be experienced by the actuator (control surface)?
Thanks





RE: Calculating Load on primary control surfaces for suitable actuator selection
RE: Calculating Load on primary control surfaces for suitable actuator selection