Aces High Bulletin Board

General Forums => The O' Club => Topic started by: Ex-jazz on January 07, 2012, 03:58:41 PM

Title: How model the accelerated stall in Flight Dynamics Model?
Post by: Ex-jazz 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?

Title: Re: How model the accelerated stall in Flight Dynamics Model?
Post by: PR3D4TOR 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)."