Hi All,
The PA-28 I normally fly has a stall speed of around 45knts in straight and level flight. What factors of an aircraft affect the stall speed? what is a 'tip stall'? I understand the basic concepts of a stall...(AOA meets a critical stage and the air flow comming off the wings is affected) can anyone expand on the definition of a stall? Is there any stage in a flight where the rear vertical stabiliser is affected by a rough airflow? Sorry if the are questions are stupid im just dumb
Can you please fill in these gaps in my brain
Many thanx
BRAD
