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rexinator(at)gmail.com Guest
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Posted: Wed Oct 31, 2007 6:38 am Post subject: Accelerated stalls |
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I decided to add a little to what Leonard has written. A wing stall
occurs any time the Angle of Attack exceeds the lift a wing can generate
regardless of airspeed. Accelerated stalls are demonstrated specifically
by putting the airplane in a 60 degree bank at a specific airspeed
(usually a slow cruise speed - Va?) while holding altitude. Properly
done this creates a 2G force which we know all aircraft should be
capable of sustaining normally. In this maneuver the aircraft should be
in balance (ball centered otherwise you can snap roll into a spin) while
the throttle is slowly decreased until stall entry is felt, then recover
from the stall. It is a maneuver taught to CFI pilots and is intended
to impress on the pilot that an airplane can stall at higher than the
airspeed published for straight and level flight. So don't try this
without an instructor or maybe a competent aerobatic check pilot.
In aerobatics the technique is used for snap rolls and other maneuvers
where you want a dramatic and quick change of attitude. Both literally
and figuratively.
So Leonard was taught part of a aerobatic technique which has probably
saved his life. This is the kind of instruction we all should have.
ref: http://en.wikipedia.org/wiki/V_speeds
http://www.auf.asn.au/groundschool/umodule2.html
--
Rex Hefferan
SE Colorado / K-II / 582-C / still waiting repairs
akflyer wrote:
Quote: |
accelerated stall is getting the plane to stall at well over stall speed.. say in a cub or something of that nature that stalls at 40-45.. you think that flying along at 75 or 80 you are safe. You see something on the ground that happens to catch your eye so you bank over and yank it around and fall out of the sky. Put your plane into a nice steep bank and start hauling the stick in your lap slowly tightening your circle, add power to keep the speed up and keep pulling the stick just like you were intently looking at something on the ground. Keep pulling the stick into your lap till you break and fall out of the sky..
A "moose hunter" stall is basically the same, but normally you are un-coordinated as you as stomping on the rudder trying to bring the nose around to so you can keep the "moose" you are looking at in view. Normally guys are low and slow out spotting and we all know what happens when you stall uncoordinated.... you will spin and are to low to recover... alot of the time guys are low enough that they hit the ground at a fairly low speed and survive the impact... only to burn up in the fire afterward. It kills ALOT of guys up here so my instructor hammered the hell out of me on both accelerated stalls and uncoordinated "moose hunter" stalls as he was well aware of the type of flying I would be doing the second he turned me loose to solo (the guy is a genius). I can tell you with a straight face that he saved my life more than once as I was doing exactly what I was trained not to do, and caught it a split second before it broke into a full spin. Had I not know what it felt l!
ike (not just "incipient") and had it burned into my brain how to recover with very minimal loss of altitude I bet I would not be typing this right now.
Whew didn't mean to get that long winded, just a subject I don't think gets put across to student pilots the way it should..
--------
Leonard Perry
Soldotna AK
Avid "C" / Mk IV
582 IVO IFA
Full Lotus 1260
95% complete
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=142902#142902
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Michel
Joined: 10 Jan 2006 Posts: 966 Location: Norway
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Posted: Wed Oct 31, 2007 7:46 am Post subject: Accelerated stalls |
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On Oct 31, 2007, at 3:36 PM, Rexinator wrote:
Quote: | an airplane can stall at higher than the airspeed published for
straight and level flight. So don't try this without an instructor or
maybe a competent aerobatic check pilot.
|
If I am not mistaking, at 60 degrees coordinated bank you endure 2 Gs
and your stall speed is increased by the square root of 2, or 1.4 times
the published straight level flight. Does that make sense?
Cheers,
Michel Verheughe
Norway
Kitfox 3 - Jabiru 2200
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akflyer
Joined: 07 May 2007 Posts: 574 Location: Soldotna AK
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Posted: Wed Oct 31, 2007 8:27 am Post subject: Re: Accelerated stalls |
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rexinator(at)gmail.com wrote: | I decided to add a little to what Leonard has written. A wing stall
occurs any time the Angle of Attack exceeds the lift a wing can generate
regardless of airspeed. Accelerated stalls are demonstrated specifically
by putting the airplane in a 60 degree bank at a specific airspeed
(usually a slow cruise speed - Va?) while holding altitude. Properly
done this creates a 2G force which we know all aircraft should be
capable of sustaining normally. In this maneuver the aircraft should be
in balance (ball centered otherwise you can snap roll into a spin) while
the throttle is slowly decreased until stall entry is felt, then recover
from the stall. It is a maneuver taught to CFI pilots and is intended
to impress on the pilot that an airplane can stall at higher than the
airspeed published for straight and level flight. So don't try this
without an instructor or maybe a competent aerobatic check pilot.
In aerobatics the technique is used for snap rolls and other maneuvers
where you want a dramatic and quick change of attitude. Both literally
and figuratively.
So Leonard was taught part of a aerobatic technique which has probably
saved his life. This is the kind of instruction we all should have.
ref: http://en.wikipedia.org/wiki/V_speeds
http://www.auf.asn.au/groundschool/umodule2.html
--
Rex Hefferan
SE Colorado / K-II / 582-C / still waiting repairs
akflyer wrote:
Quote: |
accelerated stall is getting the plane to stall at well over stall speed.. say in a cub or something of that nature that stalls at 40-45.. you think that flying along at 75 or 80 you are safe. You see something on the ground that happens to catch your eye so you bank over and yank it around and fall out of the sky. Put your plane into a nice steep bank and start hauling the stick in your lap slowly tightening your circle, add power to keep the speed up and keep pulling the stick just like you were intently looking at something on the ground. Keep pulling the stick into your lap till you break and fall out of the sky..
A "moose hunter" stall is basically the same, but normally you are un-coordinated as you as stomping on the rudder trying to bring the nose around to so you can keep the "moose" you are looking at in view. Normally guys are low and slow out spotting and we all know what happens when you stall uncoordinated.... you will spin and are to low to recover... alot of the time guys are low enough that they hit the ground at a fairly low speed and survive the impact... only to burn up in the fire afterward. It kills ALOT of guys up here so my instructor hammered the hell out of me on both accelerated stalls and uncoordinated "moose hunter" stalls as he was well aware of the type of flying I would be doing the second he turned me loose to solo (the guy is a genius). I can tell you with a straight face that he saved my life more than once as I was doing exactly what I was trained not to do, and caught it a split second before it broke into a full spin. Had I not know what it felt l!
ike (not just "incipient") and had it burned into my brain how to recover with very minimal loss of altitude I bet I would not be typing this right now.
Whew didn't mean to get that long winded, just a subject I don't think gets put across to student pilots the way it should..
--------
Leonard Perry
Soldotna AK
Avid "C" / Mk IV
582 IVO IFA
Full Lotus 1260
95% complete
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=142902#142902
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on the bold... it used to be that you were taught full on fall out of the sky stalls and spins... The government in their infinite wisdom decided that this was not good and now you are only taught to recover at the first signs of a buffet not letting it get into a full stall. I think this is a HUGE mistake as I think every pilot out there should be taught, at a bare minimum spin recovery techniques. I bet alot of guys would still be around that spun in a kitfox if they knew without hesitation that they had to take the stick outa their lap to recover. When you are low to the ground the first instinct is to try and pull the nose up...so they spin all the way in, when in fact, they could have recovered, change shorts then gone and had a beer to calm the nerves.
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_________________ DO NOT ARCHIVE
Leonard Perry aka SNAKE
Soldotna AK
Avid "C" / Mk IV
582 (147 hrs and counting on the rebuild)
IVO IFA
Full Lotus 1450
#1 snake oil salesman since 1-22-2009
I would rather die trying to live, than to live trying not to die.... |
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rexinator(at)gmail.com Guest
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Posted: Wed Oct 31, 2007 10:39 am Post subject: Accelerated stalls |
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I totally agree with Leonard that all pilots ought to know how to
recover from a spin. Some pilots are afraid to be in unusual attitudes
and perhaps would not become pilots if it were a requirement. That may
be the reason it was decided it was better not to require such training
and just the avoidance. Plus from what I was told there were more
training crashes years ago when it was included.
This way more certified pilots are created and it's been left up to the
individual to advance their training. Probably more of a political
decision than a wise one. I would encourage all pilots to learn how
handle unusual attitudes or at least continue training and include
commercial manuevers which would increase their feel for the aircraft
they fly. However, probably spins are something only risk taking
personalities want to persue, but it should not be that way. Properly
done in the proper airplane it's safe and gentle, although seeing the
ground fill the view out of your windshield while spinning will shock
most people at first it's just something to get used to. Once you know
what to expect and can correct it on your own it can become just another
skill.
Michel Verheughe wrote:
If I am not mistaking, at 60 degrees coordinated bank you endure 2 Gs
and your stall speed is increased by the square root of 2, or 1.4 times
the published straight level flight. Does that make sense?
Michel, the link below addresses the formula and states it to be 1.41 x
Vs (the published straight level flight stall), but you are close enough.
http://www.auf.asn.au/groundschool/umodule2.html#accel_stall
--
Rex Hefferan
SE Colorado / K-II / 582-C / still waiting repairs
akflyer wrote:
Quote: | on the bold... it used to be that you were taught full on fall out of the sky stalls and spins... The government in their infinite wisdom decided that this was not good and now you are only taught to recover at the first signs of a buffet not letting it get into a full stall. I think this is a HUGE mistake as I think every pilot out there should be taught, at a bare minimum spin recovery techniques. I bet alot of guys would still be around that spun in a kitfox if they knew without hesitation that they had to take the stick outa their lap to recover. When you are low to the ground the first instinct is to try and pull the nose up...so they spin all the way in, when in fact, they could have recovered, change shorts then gone and had a beer to calm the nerves.
--------
Leonard Perry
Soldotna AK
Avid "C" / Mk IV
582 IVO IFA
Full Lotus 1260
95% complete
|
--
Rex Hefferan
SE Colorado / K-II / 582-C / still waiting repairs
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Michel
Joined: 10 Jan 2006 Posts: 966 Location: Norway
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Posted: Wed Oct 31, 2007 12:01 pm Post subject: Accelerated stalls |
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On Oct 31, 2007, at 7:37 PM, Rexinator wrote:
Quote: | Michel, the link below addresses the formula and states it to be 1.41
x Vs (the published straight level flight stall), but you are close
enough.
|
Yes Rex, but I prefer to remember it as I wrote it: The square root of
the Gs.
1.4, 1.41 or 1.414213562373 are all the square root of two, but at
different resolutions.
Cheers,
Michel Verheughe
Norway
Kitfox 3 - Jabiru 2200
Do not archive
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dave
Joined: 22 Sep 2006 Posts: 1382
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Posted: Wed Oct 31, 2007 12:24 pm Post subject: Re: Accelerated stalls |
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Ok i recall talking about stalls and spins last year so I looked it up.
Here you go this will save me from typing it all in again
Cheers
http://forums.matronics.com/viewtopic.php?t=12156
dave(at)cfisher.com
Guest
Posted: Fri Jul 28, 2006 7:27 pm Post subject: Stall in a side slip
--------------------------------------------------------------------------------
Good info there Dave.
I have had spin training and I am not sure why it is not part of every
flight test anymore.
In Canada you only have to demonstrate spins for commerical and instructor
rating.
Private pilot license you used to have to as well. Why not now ? I have no
idea.
Personally I think all pilots should be tested on their flight reviews and
on flight tests the following,
Stalls,(stall on take off and approach) Spins ( fully developed) , Spirals,
unusual attitudes and alot of slow fight.
And of course recovery from all the above.
And how about turning final at approach speed and going inverted ? There
are deaths from the above every year that could be prevented.
Dave
dave(at)cfisher.com
Guest
Posted: Fri Jul 28, 2006 10:00 pm Post subject: Stall in a side slip
--------------------------------------------------------------------------------
Wake turbulence is one way but you usually have enough separation on final
.( I did have this one during IFR training under the hood) One scenario is
if one was on base turning final and you are tight and wide. So you add
more rudder and get more turn and more bank and use opposite aileron to
lessen the bank and you are low and give aft stick then see what happens
before you splat into ground.
I land nearly fully stalled in Kitfox every time on grass, pavement snow,ice
or water. I will take a high glideslope if landing behind a heavy and land
beyond their touchdown. In Kitfox I rarely get behind heavies though. I
most likely fly through my own wake turbulence more than anyone elses when
horsing around
And dead stick landings , certainly another good thing to learn. If you
have not done any well you have not learnt yet. It can happen at anytime.
i.e. bird strike,engine out , prop failure etc. Failure to leave your
self an out will not leave you an "out" .
Dave
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MichaelGibbs(at)cox.net Guest
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Posted: Wed Oct 31, 2007 7:38 pm Post subject: Accelerated stalls |
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Rex sez:
Quote: | ...from what I was told there were more training crashes years ago
when [spinning] was included.
|
When I went to get my tail wheel endorsement I started flying with a
very old fella in an Aeronca Champ. The first time I talked to him
he said, "Well, first we'll get you familiar with the plane, go out
and do some stalls and spins, then come back and work on landing and
taking off."
I told him one of my instructors had demonstrated one once but that I
had never done a spin myself.
He said, "You will today!" And we did. A whole bunch of them. It
was great fun, actually.
When I finished my Kitfox and had run through the gamut of power-on
and power-off stalls I decided it was time to spin it. My short-wing
Model IV would only spin if you held the stick full aft and kept
rudder into the turn. If you relaxed either it would accelerate into
a spiral dive. Even then, I could only get it to stay in for about
3/4 turn before it accelerated to flying speed on its own.
I think this was because it didn't have enough elevator authority to
keep it at stall speed. It was difficult to get a power-on stall to
happen at all because it would run out of up elevator--you had to
pull it sharply up to get a break to occur.
Mike G.
N728KF
Phoenix, AZ
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Float Flyr
Joined: 19 Jul 2006 Posts: 2704 Location: Campbellton, Newfoundland
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Posted: Thu Nov 01, 2007 6:53 am Post subject: Accelerated stalls |
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The flight school I trained with teaches mostly commercial pilots. It is part of their syllabus that they teach turning stalls, straight forward departure stalls, arrival stalls and spins up to insipid ( no more than four turns before correction).
I had done what I was told was a hammerhead turn (stall/spin with 180 degree turn only) but the first time the instructor put me into a spin my heart skipped a beat... I hate roller coasters but I loved that. It is so easy to see that if you have never been there you can get into a lot of trouble a lot of fast. One thing is the first thing coming to most people would be to add aileron control exaggerating the spin.
Rules at the flight school only allowed students to do spins with an instructor in the aircraft with them. Even the instructors were supposed to have a second with them while doing spins.
I agree with teaching full spin recovery! One less surprise to have.
On the other hand I fly my Kitfox so far into the envelope I doubt I'll ever have a spin. I have yet to stall it. Only because I haven't had what I consider enough altitude for safety.
[img]cid:380144914(at)01112007-2DD1[/img]
Noel Loveys, RPP, AME intern
Campbellton, Newfoundland,
Canada
Kitfox Mod III-A, 582, B box, Ivo IFA
Aerocet 1100s
noelloveys(at)yahoo.ca (noelloveys(at)yahoo.ca)
[quote] > > accelerated stall is getting the plane to stall at well
over stall speed.. say in a cub or something of that nature
that stalls at 40-45.. you think that flying along at 75 or
80 you are safe. You see something on the ground that
happens to catch your eye so you bank over and yank it around
and fall out of the sky. Put your plane into a nice steep
bank and start hauling the stick in your lap slowly
tightening your circle, add power to keep the speed up and
keep pulling the stick just like you were intently looking at
something on the ground. Keep pulling the stick into your
lap till you break and fall out of the sky..
> >
> > A "moose hunter" stall is basically the same, but
normally you are un-coordinated as you as stomping on the
rudder trying to bring the nose around to so you can keep the
"moose" you are looking at in view. Normally guys are low
and slow out spotting and we all know what happens when you
stall uncoordinated.... you will spin and are to low to
recover... alot of the time guys are low enough that they hit
the ground at a fairly low speed and survive the impact...
only to burn up in the fire afterward. It kills ALOT of guys
up here so my instructor hammered the hell out of me on both
accelerated stalls and uncoordinated "moose hunter" stalls as
he was well aware of the type of flying I would be doing the
second he turned me loose to solo (the guy is a genius). I
can tell you with a straight face that he saved my life more
than once as I was doing exactly what I was trained not to
do, and caught it a split second before it broke into a full
spin. Had I not know what it fe!
lt l!
> > ike (not just "incipient") and had it burned into my
brain how to recover with very minimal loss of altitude I bet
I would not be typing this right now.
> >
> > Whew didn't mean to get that long winded, just a subject
I don't think gets put across to student pilots the way it should..
> >
> > --------
> > Leonard Perry
> > Soldotna AK
> > Avid "C" / Mk IV
> > 582 IVO IFA
> > Full Lotus 1260
> > 95% complete
> >
> >
> >
> >
> > Read this topic online here:
> >
> > http://forums.matronics.com/viewtopic.php?p=142902#142902
> >
> >
> >
> >
>
on the bold... it used to be that you were taught full on
fall out of the sky stalls and spins... The government in
their infinite wisdom decided that this was not good and now
you are only taught to recover at the first signs of a buffet
not letting it get into a full stall. I think this is a HUGE
mistake as I think every pilot out there should be taught, at
a bare minimum spin recovery techniques. I bet alot of guys
would still be around that spun in a kitfox if they knew
without hesitation that they had to take the stick outa their
lap to recover. When you are low to the ground the first
instinct is to try and pull the nose up...so they spin all
the way in, when in fact, they could have recovered, change
shorts then gone and had a beer to calm the nerves.
--------
Leonard Perry
Soldotna AK
Avid "C" / Mk IV
582 IVO IFA
Full Lotus 1260
95% complete
Read this topic online here:
http://forums.matronics.com/viewtopic.php?p=142958#142958
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Kitfox III-A
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ruebd(at)skymail.csus.edu Guest
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Posted: Thu Nov 01, 2007 12:21 pm Post subject: Accelerated stalls |
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List:
I will put my two cents worth in on this one, since I do
distinctly remember what my late instructor, one James Hackney, had to
say on the subject in the mid 1970's, when I was studying with him for
advanced ratings under the G.I. bill.
He explained that an accelerated stall was produced by curving
the path of the wing, which then produced load factors greater than one.
Notice that nothing is said about the bank angle in this, and, indeed
doesn't need to be. (The reference load factor of one, being generated
by flying straight and level in calm air.) At first my engineering self
wanted this to be too simple an explanation, and I was searching for the
flaw in this simple explanation, but I still after all these years
cannot find any fault with Jim's brilliantly simple and therefore
elegant explanation.
If anyone out there can see a problem with this, please tell us
all.
Duane Rueb, N24ZM
--
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akanka(at)kiamichiwb.org Guest
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Posted: Thu Nov 01, 2007 1:14 pm Post subject: Accelerated stalls |
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If curving the path of an airfoil (wing) produces an accelerated stall, how
come helicopter airfoils (blades) produce lift? They run in a continuous
circle (curved path), and the load factor on them change continuously due to
changing angle of attack in the plane of rotation to compensate for
dissymmetry of lift caused by the advancing half of the rotor system's
relative wind equaling the rotational speed plus the forward airspeed while
the retreating half's relative wind is the rotational speed minus the
forward airspeed.
FAA AC 61-67C with Change 1, Subject: Stall and Spin Awareness Training, is
located online at
http://rgl.faa.gov/Regulatory_and_Guidance_Library/rgAdvisoryCircular.nsf/0/
543ceffb938738a28625736100575511/$FILE/AC%2061-67C%20%20CHG%201.pdf
For what it's worth, FAA AC No: 61-67C, paragraph 104 is quoted below:
104. TYPES OF STALLS. Stalls can be practiced both with and without power.
Stalls should be
practiced to familiarize the student with the aircraft's particular stall
characteristics without putting
the aircraft into a potentially dangerous condition. In multiengine
airplanes, single-engine stalls
must be avoided. Descriptions of some different types of stalls follows:
a. Power-off stalls (also known as approach-to-landing stalls) are practiced
to simulate
normal approach-to-landing conditions and configuration. Many stall/spin
accidents have occurred
in these power-off situations, such as crossed control turns from base leg
to final approach
(resulting in a skidding or slipping turn); attempting to recover from a
high sink rate on final
approach by using only an increased pitch attitude; and improper airspeed
control on final approach
or in other segments of the traffic pattern.
b. Power-on stalls (also known as departure stalls) are practiced to
simulate takeoff and
climbout conditions and configuration. Many stall/spin accidents have
occurred during these phases of flight, particularly during go-arounds. A
causal factor in such accidents has been the pilot's
failure to maintain positive control due to a nose-high trim setting or
premature flap retraction, and
during short field takeoffs has also been a causal accident factor.
c. Accelerated stalls can occur at higher-than-normal airspeeds due to
abrupt and/or excessive
control applications. These stalls may occur in steep turns, pullups, or
other abrupt changes in
flightpath. Accelerated stalls usually are more severe than unaccelerated
stalls and are often
unexpected because they occur at higher-than-normal airspeeds.
John Hart
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wingnut
Joined: 11 Jan 2006 Posts: 356
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Posted: Thu Nov 01, 2007 1:52 pm Post subject: Re: Accelerated stalls |
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What does it mean to curve the path of a wing?
The best explanation of the physics of a stall that I know focuses on angle of attack which is the angle of the incidence of the airfoil relative to the direction its moving through the air. In fact, isn't that what stall/lift reserve indicators actually measure? If your angle of attack gets too high the flow of air separates from the top of the airfoil and it looses it's ability to produce lift. The same principal applies to helicopter blades as well.
Quote: | He explained that an accelerated stall was produced by curving
the path of the wing, which then produced load factors greater than one. |
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_________________ Luis Rodriguez
Model IV 1200
Rotax 912UL
Flying Weekly
Laurens, SC (34A) |
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wingnut
Joined: 11 Jan 2006 Posts: 356
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Posted: Thu Nov 01, 2007 2:01 pm Post subject: Re: Accelerated stalls |
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On the other hand, while talking about the physics behind a stall might be interesting and maybe even enlightening, I think it's still worth talking about the various situations where a high angle of attack occurs. After all, people might not make the connection in their minds between what they they're doing and the aerodynamic consequences.
Steep turns during slow flight seem to me like one of the more popular ways that pilots induce high angles of attack. I read posts on this very forum from time to time that seem to advocate the practice.
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_________________ Luis Rodriguez
Model IV 1200
Rotax 912UL
Flying Weekly
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ruebd(at)skymail.csus.edu Guest
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Posted: Thu Nov 01, 2007 2:18 pm Post subject: Accelerated stalls |
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What it means to curve the path of the wing is to cause it to curve by
first banking and turning (a curve) or by abruptly causing it to climb,
(a curve), and this is true for both a positive curve or a negative one.
As long as there is a curved path, the load factor will be other than
one. With a negative curve established from straight and level flight,
the load factor will first be reduced below one. But the key to how
much load factor is in how much of a curve, and what the airspeed is.
But the path needs to curve for this to happen. Even in turbulence
where you are attempting straight and level flight, the air that causes
you to experience high and low load factors is causing a curved path of
the aircraft. Note that nothing is said about angle of attack, but of
course it follows that this will be changing to compensate for the
curved path involved when the load factor deviates from one.
Duane Rueb, N24ZM
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wingnut
Joined: 11 Jan 2006 Posts: 356
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Posted: Thu Nov 01, 2007 3:24 pm Post subject: Re: Accelerated stalls |
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OK. Now that I understand curving the path of a wing meens, I'd have to say that this doesn't seem to me like a good description of what is going on in a stall at all. An airfoil can be stalled with no 'curve' to it's direction of travel at all and a load factor of even less than 1. Consider this, if you kill your engine, the airplane will begin to slow down. As it slows down and begins to loose lift, you can pull back slowly to maintain a strait flight (ie: no curve). Eventually, the airplane is going to stall. Guess what you have when the airplane finally stalls? You guessed it, a high angle of attack.
Quote: | What it means to curve the path of the wing is to cause it to curve by first banking and turning (a curve) or by abruptly causing it to climb,
(a curve), and this is true for both a positive curve or a negative one.
As long as there is a curved path, the load factor will be other than
one. With a negative curve established from straight and level flight,
the load factor will first be reduced below one. But the key to how
much load factor is in how much of a curve, and what the airspeed is. |
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_________________ Luis Rodriguez
Model IV 1200
Rotax 912UL
Flying Weekly
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rexinator(at)gmail.com Guest
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Posted: Thu Nov 01, 2007 3:51 pm Post subject: Accelerated stalls |
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I'm not so sure if describing an acellerated stall as curving the path
of the wing works as well in text form. If you are showing what you mean
with hand gestures or a model aircraft it would work better. Which is
always true describing flight, a visual image helps greatly. Here's
another attempt.
Any stall occurs when Angle of Attack referenced to relative wind
exceeds the lift capability of the airfoil.
I used "airfoil" here to allow the statement to apply to elevators and
propellers as well. Seems better to me. No reference to bank angle there
and as you said it doesn't need to be. A stall can occur regardless of
the path of flight, but gravity and bank angle effects the lift capacity
(G load) as compared to wings level. Thus the practice of using a 60
degree bank angle. Lift capacity is reduced in the 60 degree
accellerated stall because of the lift vector in relation to gravity so
that structual damage is not possible at the speeds used.
I should note that it used to be the FARs allowed certain training
manuevers with a CFI that would normally fall under the definition of
"aerobatic flight" without the requirement of parachutes. An
accellerated stall without a CFI would have been defined as a aerobatic
maneuver. I'm not sure what the regs say now.
Rex Hefferan
Rueb, Duane wrote:
Quote: |
List:
I will put my two cents worth in on this one, since I do
distinctly remember what my late instructor, one James Hackney, had to
say on the subject in the mid 1970's, when I was studying with him for
advanced ratings under the G.I. bill.
He explained that an accelerated stall was produced by curving
the path of the wing, which then produced load factors greater than one.
Notice that nothing is said about the bank angle in this, and, indeed
doesn't need to be. (The reference load factor of one, being generated
by flying straight and level in calm air.) At first my engineering self
wanted this to be too simple an explanation, and I was searching for the
flaw in this simple explanation, but I still after all these years
cannot find any fault with Jim's brilliantly simple and therefore
elegant explanation.
If anyone out there can see a problem with this, please tell us
all.
Duane Rueb, N24ZM
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Rex Hefferan
SE Colorado / K-II / 582-C / still waiting repairs
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avidfox
Joined: 03 Apr 2007 Posts: 87
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Posted: Thu Nov 01, 2007 4:13 pm Post subject: Accelerated stalls |
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§ 91.303 Aerobatic flight.
No person may operate an aircraft in aerobatic flight—
(a) Over any congested area of a city, town, or settlement;
(b) Over an open air assembly of persons;
(c) Within the lateral boundaries of the surface areas of Class B, Class C, Class D, or Class E airspace designated for an airport;
(d) Within 4 nautical miles of the center line of any Federal airway;
(e) Below an altitude of 1,500 feet above the surface; or
(f) When flight visibility is less than 3 statute miles.
For the purposes of this section, aerobatic flight means an intentional maneuver involving an abrupt change in an aircraft's attitude, an abnormal attitude, or abnormal acceleration, not necessary for normal flight.
§ 91.307 Parachutes and parachuting.
(c) Unless each occupant of the aircraft is wearing an approved parachute, no pilot of a civil aircraft carrying any person (other than a crewmember) may execute any intentional maneuver that exceeds—
(1) A bank of 60 degrees relative to the horizon; or
(2) A nose-up or nose-down attitude of 30 degrees relative to the horizon.
(d) Paragraph (c) of this section does not apply to—
(1) Flight tests for pilot certification or rating; or
(2) Spins and other flight maneuvers required by the regulations for any certificate or rating when given by—
(i) A certificated flight instructor; or
(ii) An airline transport pilot instructing in accordance with §61.67 of this chapter.
[quote][b]
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nail13zg(at)centurytel.ne Guest
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Posted: Thu Nov 01, 2007 4:17 pm Post subject: Accelerated stalls |
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Curves and airspeed, etc. etc. I think we are missing a fundamental lesson here on stalls. An airplane, any airplane, stalls when the wing's designed critical angle of attack is exceeded. For most general aviation airplanes this angle is about 18 degrees. When this angel of attack is exceeded, regardless of airspeed, weight, configuration, attitude, or anything else you can think of, the wing stalls.
Trey Moran
[quote][b]
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dgolden(at)golden-consult Guest
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Posted: Fri Nov 02, 2007 12:31 pm Post subject: Accelerated stalls |
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Rueb, Duane wrote:
Quote: |
List:
I will put my two cents worth in on this one, since I do
distinctly remember what my late instructor, one James Hackney, had to
say on the subject in the mid 1970's, when I was studying with him for
advanced ratings under the G.I. bill.
He explained that an accelerated stall was produced by curving
the path of the wing, which then produced load factors greater than one.
Notice that nothing is said about the bank angle in this, and, indeed
doesn't need to be. (The reference load factor of one, being generated
by flying straight and level in calm air.) At first my engineering self
wanted this to be too simple an explanation, and I was searching for the
flaw in this simple explanation, but I still after all these years
cannot find any fault with Jim's brilliantly simple and therefore
elegant explanation.
If anyone out there can see a problem with this, please tell us
all.
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After I left the service, I was training at a Part 141 school. They
taught accelerated stalls by stalling right after recovering from a
departure stall. This was in a Cherokee 140 and was quite dramatic.
Dennis
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Dennis Golden
Golden Consulting Services, Inc.
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