SixPapaCharlie
May the force be with you
- Joined
- Aug 8, 2013
- Messages
- 16,541
- Display Name
Display name:
Sixer
The Cirrus thread got me thinking.
I have not dug deep into what the plane goes through during a stall
I would figure it was somewhere between 0-1 G then maybe a fraction above 1 G on the recovery. I dunno. Just guessing there.
Then Ron mentioned something called a Whip stall which I have yet to google. He stated that that is prohibited. I am guessung that maneuver stresses the airframe or maybe is more likely to put it into a spin?
So, two questions I guess:
1. What is with Whip stalls. What are they? Why would they be prohibited?
2. When just out practicing power on / power off stalls are you adding any stress to the airframe beyond normal cruise maneuvers?
Thanks.
I have not dug deep into what the plane goes through during a stall
I would figure it was somewhere between 0-1 G then maybe a fraction above 1 G on the recovery. I dunno. Just guessing there.
Then Ron mentioned something called a Whip stall which I have yet to google. He stated that that is prohibited. I am guessung that maneuver stresses the airframe or maybe is more likely to put it into a spin?
So, two questions I guess:
1. What is with Whip stalls. What are they? Why would they be prohibited?
2. When just out practicing power on / power off stalls are you adding any stress to the airframe beyond normal cruise maneuvers?
Thanks.