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Aerodynamic qualities by geographic location

 
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Non Compis Mentis
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PostPosted: Sun Apr 04, 2004 11:49 am    Post subject: Aerodynamic qualities by geographic location Reply with quote



Folks,

A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?

Reason why I ask it is because of the different methods taught of stall
recovery of the same a/c type in different countries/schools.

e.g. PA28-161 - stall clean: In Aus - Throttle off, release back
pressure, flying speed (60KIAS?), apply throttle and climb out..

UK: full throttle, release back pressure but maintain height - when
enough a/s, fly away... (at least 2 organisation taught it this way).

I know which one I generally prefer, but why the difference for the same
a/c type?

NCM
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Stealth Pilot
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PostPosted: Sun Apr 04, 2004 12:58 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote



On Sun, 04 Apr 2004 21:49:55 +1000, Non Compis Mentis
<ncm (AT) somewhere (DOT) com> wrote:

Quote:
Folks,

A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?

Reason why I ask it is because of the different methods taught of stall
recovery of the same a/c type in different countries/schools.

e.g. PA28-161 - stall clean: In Aus - Throttle off, release back
pressure, flying speed (60KIAS?), apply throttle and climb out..

UK: full throttle, release back pressure but maintain height - when
enough a/s, fly away... (at least 2 organisation taught it this way).

I know which one I generally prefer, but why the difference for the same
a/c type?

NCM

not enough data points for a valid sample.
I think your australian example is an anomalous one.
the uk procedure is the correct one for recovery from an incipient
stall with zero or minimal loss of height.
I use it in the tailwind as well.

(only exception would be an aircraft such as a P51 with enormous
amounts of torque, then you'd bleed in the power gradually.)

regulatory differences used to exist but australia has abandoned the
local quaintness for the manufacturers original operating
instructions.

btw there are performance variations actually due to geographic
locations though not what you are alluding to. there is a map in the
aip's I think which gives standardised figures for density height by
season across australia. ground elevation, temperature, density and
humidity are the factors.
Stealth Pilot

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Centurion
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PostPosted: Sun Apr 04, 2004 2:55 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote



Stealth Pilot wrote:

Quote:
On Sun, 04 Apr 2004 21:49:55 +1000, Non Compis Mentis
[email]ncm (AT) somewhere (DOT) com[/email]> wrote:

Folks,

A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?

Reason why I ask it is because of the different methods taught of stall
recovery of the same a/c type in different countries/schools.

e.g. PA28-161 - stall clean: In Aus - Throttle off, release back
pressure, flying speed (60KIAS?), apply throttle and climb out..

UK: full throttle, release back pressure but maintain height - when
enough a/s, fly away... (at least 2 organisation taught it this way).

I know which one I generally prefer, but why the difference for the same
a/c type?

NCM

not enough data points for a valid sample.
I think your australian example is an anomalous one.
the uk procedure is the correct one for recovery from an incipient
stall with zero or minimal loss of height.
I use it in the tailwind as well.

(only exception would be an aircraft such as a P51 with enormous
amounts of torque, then you'd bleed in the power gradually.)

P51's and lightly loaded C208B's Smile When I did my endorsement on the Grand
Caravan we did some incipient stalls just to see what happens etc.

The problem with the Caravan is lack of aileron authority leading up to the
stall - you're dancing on the rudder pedals for the last couple of kias!

Anyway, the stall warning goes off, VSI goes south. So you grab the power
lever and push it smartly to about 3/4 position (still dancing on the
rudder pedals), the PT6 spools up (surges a little if you've been rough)
then holey snapping duck crap(!) the torque kicks in and you get the wing
drop from hell. Boot full of top rudder (pushed to the firewall) and the
wing doesn't drop any further but you're in stall recovery with about 30-45
degrees of bank!

Good fun really :)

James
--
Fortune cookies says:
BOFH excuse #186:

permission denied


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Peter Creswick
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PostPosted: Sun Apr 04, 2004 3:40 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote

Stealth, try use of power to recover from a stall, or incipient stall, in a
glider.
OK, back to square one.
Aerodynamic stalls have to be aerodynamically unstalled, no other means will do.
Teaching use of power, specifically increasing power, and even worse, teaching
holding, or attempting to hold height, apparently by minimal release of back
pressure, as a part of the procedure, is a recipe for disaster, and may indeed
be the root cause of most lightie low altitude, low speed, and final turn
stall-spin-crunch accidents. People are being trained WRONG thinking.
For my money, you want to get the wing unstalled, which means change the angle
of attack of the relative airflow downwards, ie, less angle / alpha, which means
pitch down, which means stick forward, all with a reasonable degree of
smoothness and deliberate but modest haste. Failing to do so only allows the
stall or incipient stall to develop further.
Playing the power game, especially with big power beasts like P-51's, with heaps
of torque, would definitely complicate the issue, facilitating torque induced
rotation, which only further worsens the situation, sending everything deep
south in a bloody big hurry.
Centurion's example is also interesting. The beginning of loss of aileron
authority also directly leads you into secondary effects land and the rapid
increase in the possibility of an aerodynamic auto rotation, not just "a wing
drop", the two are different beasts remember, let alone the torque effects.
Dancing on the pedals during this time of the last few knots is also fun as
Centurion points out.
I had a lot of fun with a Blanik in this regard. I was minimum weight (150 lbs)
for the front seat solo with no ballast, so I was able to fly the blanik at
lowest AUW and on the aft CG limit. One day, I decided to see what the absolute
minimum speed was before it all went south. With full flap, and bringing the
speed back ever so slowly, and knowing the ailerons gave some secondary effects
at about 38 kias, I held stick centre, and "walked the rudder" into a mushing
stall, all the way down to 32 kias, before going south, which was a straight
pitch nose down 2 out of 3 times. Once, it went into a full blooded auto rotate
and spin, requiring standard recovery (heave the pink handle fully forward as
soon as it started to roll) but I think it was caused by a bit of a gust, ie, it
was not something a blanik would do by itself, ie, normally you had to force her
to auto rotate by a deliberate slight nose high stall complete with out stick
and a nudge or more of in rudder to get her to go over, and when it did, it
really did !
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Ted Harrison
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PostPosted: Sun Apr 04, 2004 9:18 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote


"Non Compis Mentis" <ncm (AT) somewhere (DOT) com> wrote

Quote:
Folks,

A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?


Not for the purpose of your example.


Quote:
Reason why I ask it is because of the different methods taught of stall
recovery of the same a/c type in different countries/schools.

e.g. PA28-161 - stall clean: In Aus - Throttle off, release back
pressure, flying speed (60KIAS?), apply throttle and climb out..


This is not an "Australian" thing. It's an individual school or instructor fad.

What was the explanation given for failing to use power (slipstream) to help
unstall the inboard (earlier stalling) sections of the wings?

Quote:
UK: full throttle, release back pressure but maintain height - when
enough a/s, fly away... (at least 2 organisation taught it this way).


I know which one I generally prefer but why the difference for the same a/c
type?


Somebody mixed stall recovery up with spin recovery?




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Martin Taylor
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PostPosted: Tue Apr 06, 2004 7:57 am    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote

Non said....

Quote:
A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?

If you're asking a rhetorical question, should you be expecting an
answer?




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RT
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PostPosted: Tue Apr 06, 2004 9:30 am    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote


Martin Taylor wrote in message <40726819.38cc1697.bm001 (AT) yahoo (DOT) com.au>...
Quote:
If you're asking a rhetorical question, should you be expecting an
answer?


Er...... is that a rhetorical question? :-)



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Non Compis Mentis
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PostPosted: Tue Apr 06, 2004 12:23 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote

Martin Taylor wrote:
Quote:
Non said....


A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?


If you're asking a rhetorical question, should you be expecting an
answer?



Not to that particular question, but to the ones following..


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Non Compis Mentis
Guest





PostPosted: Tue Apr 06, 2004 12:27 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote

Non Compis Mentis wrote:
Quote:
Folks,

A rhetorical question, but all other things being constant, do
aerodynamic qualities of an aircraft change by geographic location?

Reason why I ask it is because of the different methods taught of stall
recovery of the same a/c type in different countries/schools.

e.g. PA28-161 - stall clean: In Aus - Throttle off, release back
pressure, flying speed (60KIAS?), apply throttle and climb out..

UK: full throttle, release back pressure but maintain height - when
enough a/s, fly away... (at least 2 organisation taught it this way).

I know which one I generally prefer, but why the difference for the same
a/c type?

NCM
Thanks for your replies,


NCM

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Stealth Pilot
Guest





PostPosted: Tue Apr 06, 2004 2:57 pm    Post subject: Re: Aerodynamic qualities by geographic location Reply with quote

On Mon, 05 Apr 2004 01:40:57 +1000, Peter Creswick
<ventus45 (AT) ihug (DOT) SOMEBODY.com.au> wrote:

Quote:
Stealth, try use of power to recover from a stall, or incipient stall, in a
glider.
who flies gliders? btw it equates to getting rid of the drag brakes.


Quote:
OK, back to square one.
Aerodynamic stalls have to be aerodynamically unstalled, no other means will do.
Teaching use of power, specifically increasing power, and even worse, teaching
holding, or attempting to hold height, apparently by minimal release of back
pressure, as a part of the procedure, is a recipe for disaster, and may indeed
be the root cause of most lightie low altitude, low speed, and final turn
stall-spin-crunch accidents. People are being trained WRONG thinking.
For my money, you want to get the wing unstalled, which means change the angle
of attack of the relative airflow downwards, ie, less angle / alpha, which means

regarding powered aircraft I dont think you are right.

the need is to be able to recover from a stall with no loss of
altitude, otherwise if you make the mistake of entering a stall on
late finals or during a go around you are dead.

in a powered aircraft you can be within a gnats whisker of the stall
and still be flying, increase the thrust on all the lighties I've
flown and you immediately fly out of the stall.
if you wait until after you get the nose drop of course then it is too
late.

in real life you never stall the aircraft unless you are doing it
deliberately. so the fly out of an impending stall technique is really
intended for the situations when you are flying slow and a loss of
situational awareness can occur. for all intending purposes you are
only slow during approach or go around and they are manouvers in close
proximity to the planetary surface, hence the zero height loss
requirement.

in the area of stalls the availability of power creates different
operational techniques between gliders and powered aircraft.
ymmv
Stealth Pilot

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