Author Topic: How model the accelerated stall in Flight Dynamics Model?  (Read 219 times)

Offline Ex-jazz

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How model the accelerated stall in Flight Dynamics Model?
« on: January 07, 2012, 03:58:41 PM »
Hi

I try to understand the basics of this phenomenon.

I was looking some real-life YT-videos and it was looking like the tail wing stalled due rash elevator input and caused a plane pitch down.

Is it that simple?


Offline PR3D4TOR

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Re: How model the accelerated stall in Flight Dynamics Model?
« Reply #1 on: January 07, 2012, 04:48:29 PM »
It's even simpler.

"An accelerated stall is a stall that occurs while the aircraft is experiencing a load factor higher than 1 (1g), for example while turning or pulling up from a dive. In these conditions, the aircraft stalls at higher speeds than the normal stall speed (which always refers to straight and level flight)."
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