Flight control surface authority question.

AI Thread Summary
Determining the authority of a flight control surface when deflected involves complex calculations that are not straightforward, as the aviation industry still faces challenges in this area. The authority can significantly vary based on airflow conditions around the control surfaces. Historical incidents, such as the loss of the prototype C130J due to inadequate control authority, highlight the importance of accurate assessments. Basic calculations serve as a starting point, but further research and refinement are necessary for reliable results. Understanding these dynamics is crucial for improving aircraft safety and performance.
Strike_42
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Hey everyone,

I'm trying to figure out what formula I would use to find the authority a flight control surface (not a wing) would have when deflected. I've been searching and searching for information, but if anyone has done some similar calculations, the help would be greatly appreciated!
 
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Not a simple question, as the industry still encounters problems here, even in fairly mature aircraft.
For instance, the prototype C130J was lost because of inadequate control authority in a flight test.
Plus the authority can vary depending on the air flow around the control surfaces.
So the basic calculations are just a beginning.
 
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