10 July 2011 cancelled due to
weather.
17 July 2011 Warrior III -
VH-TXH
In 12 years of paragliding I'd never intentional
stall my paraglider - probably because it collapses into a ball above your head
and all hell breaks loose. But now I had to make a plane stop flying and
fall out of the sky.
My lesson is booked for Sunday 10th July but when I
wake up and look out the window and it looks like the weather gods have decided
I have to wait another week. My first cancelled lesson.
Stall by Jetfxer |
The next week comes around and the weather is looking
much better but when I arrived at the airport, I find out Jason is running very
late and won't be able to make my lesson. I'm starting to think this was not
meant to be.
Luckily Fenella has some time before her first
lesson, so I’m not going to get out of it - to be honest I was hanging out for
a fly. So once again I’m with a different instructor.
We take-off and head to the training area and it’s
time.
- HASEL check – Height, Area, Secure, Engine and
Lookout,
- Carb heat on, Power to idle,
- Keep pulling back to try and maintain height until,
- The stall alarm starts going off, Carb heat off,
- The buffering starts then plane stops flying and
nose drops
- Let it drop, apply full power, keep it straight
with the rudder
- As the speed builds level out and return to
Straight and level flight.
THAT’S IT??? Clearly I’ve seen too many airshows.
While I wasn’t expecting a hammer head stall, I was expecting a bit more of a
reaction.
The next few were much the same non-event. We did have one small wing drop but had
it quickly under control with opposite rudder.
All in all, another fun day of flying.
Piper Warrior III VH-TXH, Flight Time 1.2hr (Total 6.7hrs)
Technical stuff
- HASEL check –
o Height - 3000Ft+
o Area – No over build up areas,
preferably lots of paddocks,
o Secure – Hatches, Harness and any
loose items away,
o Engine – Oil Temp & Pressure,
Fuel Pressure, fuel pump on, carb heat on, and
o Lookout 360O clearing
turn, (follow by 90O turn after each stall)
- For the
Warrior III VS1 (Clean Stall Speed) = 50KIAS and VS0
(Stall Speed with full flaps) =44KIAS
- The Stall
angle of attack doesn’t change. How the
Stall speed does.
- Stall
Speed is effected by
1. Weight – VS0
and VS1 are measured at Maximum weight. The stall speed will be lower when the plane
is lighter.
VS = √(current weight/Maximum
weight) X VS(max weight)
2. Change in wing lift profile Ie Using Flaps, Slats, Damage to the wing, Icing etc. As an example applying flaps increases the
lift produced by the wing for the same angle of attack. Icing on the other hand decrease the lift
produced by the wing.
3. Dynamic wing loading. The stall
stall increases by 2 main manoeuvres
to watch out for
a. Turns In a turn
the lift vector is banked, so more lift is required counter the weight of the
aircraft. Eg in a 60% bank the load
factor is 2. Increase in stall speed is √load
factor ie. √2 =1.414.
b. Drive recovery. Eg in a
2G pull out the load factor is 2 so once again increase in stall speed is √load
factor ie. √2 =1.414.
4. Use of Power.
a. Increasing power increases the
airflow over the wing root and hence generates more lift. It also acts at a lower angle of attack.
b. In a climb the power trust line
is inclined and the vertical component therefore helps “lift” the plane.
- DON’T use the ailerons to pick up a Drop wing at the point of stall. Using ailerons to try and level the plane
will only increase the angle of attack of the dropped wing further. This will further stall the dropped wing making it worst. Use the rudder instead. The secondary effect of yawing is roll.
- As the Angle of attack increases the Centre of
Pressure Cp moves forward. At
the point of stall it moves rapidly backwards, which causes the nose to drop
(Which is a good thing)
- HASEL check –
VS = √(current weight/Maximum weight) X VS(max weight)
- DON’T use the ailerons to pick up a Drop wing at the point of stall. Using ailerons to try and level the plane will only increase the angle of attack of the dropped wing further. This will further stall the dropped wing making it worst. Use the rudder instead. The secondary effect of yawing is roll.
- As the Angle of attack increases the Centre of Pressure Cp moves forward. At the point of stall it moves rapidly backwards, which causes the nose to drop (Which is a good thing)