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visualisation of the lift distribution over a wing



 
 
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  #1  
Old December 2nd 09, 06:58 PM posted to rec.aviation.homebuilt
Alan Baker
external usenet poster
 
Posts: 244
Default visualisation of the lift distribution over a wing

In article ,
Jim Logajan wrote:

Alan Baker wrote:
In article ,
Jim Logajan wrote:

Alan Baker wrote:
Because the push is caused by the impact of countless air molecules
with the surface of wing. If those collisions fall to zero (i.e. in
a perfect vacuum) then there is zero push.

I don't see what a change in air density (such as taking the extreme
case of a vacuum) has to do with lift. Unless you are claiming
density change as a requirement?

I believe lift can be reasonably computed using inviscid
_incompressible_ flow theory (e.g. as far back as Kutta's 1902
dissertation,) so I don't see why any change in _density_ - much less
the vacuum edge case - needs to be invoked.


Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.


That assertion is incorrect. You are no dummy so I'm sure you'll correct it
when you realize the errors.


Sorry, but it's not. Pressure is created by particle collisions.


I never mentioned density.


Sorry, but you used the word "vacuum." The notable characteristic of a
vacuum is that its density is zero.


That is *a* notable characteristic.

--
Alan Baker
Vancouver, British Columbia
http://gallery.me.com/alangbaker/100008/DSCF0162/web.jpg
  #2  
Old December 3rd 09, 01:07 AM posted to rec.aviation.homebuilt
Brian Whatcott
external usenet poster
 
Posts: 915
Default visualisation of the lift distribution over a wing

Alan Baker wrote:
In article ,
Jim Logajan wrote:


Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.


That assertion is incorrect. You are no dummy so I'm sure you'll correct it
when you realize the errors.


Sorry, but it's not. Pressure is created by particle collisions.


Hmmm...looks like Jim expected too much from you: the kinetic theory of
gases has it that pressure may be computed from the temperature AND the
density of gases... that is to say, by retaining the SAME molar quantity
of gas, and raising its temperature (which translates to a higher
velocity), the pressure is increased P.V = R.t and all that....

Put it another way: each "hotter" molecule reverses direction at a
surface with greater force.

Brian W
  #3  
Old December 3rd 09, 01:14 AM posted to rec.aviation.homebuilt
Alan Baker
external usenet poster
 
Posts: 244
Default visualisation of the lift distribution over a wing

In article ,
brian whatcott wrote:

Alan Baker wrote:
In article ,
Jim Logajan wrote:


Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.


That assertion is incorrect. You are no dummy so I'm sure you'll correct
it
when you realize the errors.


Sorry, but it's not. Pressure is created by particle collisions.


Hmmm...looks like Jim expected too much from you: the kinetic theory of
gases has it that pressure may be computed from the temperature AND the
density of gases... that is to say, by retaining the SAME molar quantity
of gas, and raising its temperature (which translates to a higher
velocity), the pressure is increased P.V = R.t and all that....

Put it another way: each "hotter" molecule reverses direction at a
surface with greater force.

Brian W


I'm perfectly aware of that, but that hardly matters for the scope of
our discussion of the effect of pressure on a wing. The point I'm making
is that all else being equal, more collisions means higher pressure and
fewer means lower pressure, but that pressure is therefore always a
positive value that acts toward the surface to which it is applied.

It is *never* acting away from that surface; i.e. "pulling".

That is the only reason I mentioned a vacuum, because it is a situation
in which there is *by definition* zero absolute pressure.

--
Alan Baker
Vancouver, British Columbia
http://gallery.me.com/alangbaker/100008/DSCF0162/web.jpg
  #4  
Old December 3rd 09, 12:54 PM posted to rec.aviation.homebuilt
Brian Whatcott
external usenet poster
 
Posts: 915
Default visualisation of the lift distribution over a wing

Alan Baker wrote:
/snip/
Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.


That assertion is incorrect. You are no dummy so I'm sure you'll correct
it when you realize the errors.


Sorry, but it's not. Pressure is created by particle collisions.


Hmmm...looks like Jim expected too much from you: the kinetic theory of
gases has it that pressure may be computed from the temperature AND the
density of gases... that is to say, by retaining the SAME molar quantity
of gas, and raising its temperature (which translates to a higher
velocity), the pressure is increased P.V = R.t and all that....

Put it another way: each "hotter" molecule reverses direction at a
surface with greater force.

Brian W


I'm perfectly aware of that...


It took me too long to realise the problem: you have a problem with
saying: "Oh yes, I got it worng."

People who WON'T do that in technical discussions qualify as people who
are just happy to stir up heated debate.

I am going to leave this thread now: wrasslin' with pigs gets the
hands jest too soiled...

Brian W
  #5  
Old December 3rd 09, 06:34 PM posted to rec.aviation.homebuilt
Alan Baker
external usenet poster
 
Posts: 244
Default visualisation of the lift distribution over a wing

In article ,
brian whatcott wrote:

Alan Baker wrote:
/snip/
Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.


That assertion is incorrect. You are no dummy so I'm sure you'll correct
it when you realize the errors.


Sorry, but it's not. Pressure is created by particle collisions.


Hmmm...looks like Jim expected too much from you: the kinetic theory of
gases has it that pressure may be computed from the temperature AND the
density of gases... that is to say, by retaining the SAME molar quantity
of gas, and raising its temperature (which translates to a higher
velocity), the pressure is increased P.V = R.t and all that....

Put it another way: each "hotter" molecule reverses direction at a
surface with greater force.

Brian W


I'm perfectly aware of that...


It took me too long to realise the problem: you have a problem with
saying: "Oh yes, I got it worng."


I didn't get anything wrong.

I am and was perfectly aware of the fact that the temperature of a gas
indicates a different average speed for the gas molecules and thus a
different momentum when the strike a surface.


People who WON'T do that in technical discussions qualify as people who
are just happy to stir up heated debate.


I agree. What of it.


I am going to leave this thread now: wrasslin' with pigs gets the
hands jest too soiled...


You can go.

--
Alan Baker
Vancouver, British Columbia
http://gallery.me.com/alangbaker/100008/DSCF0162/web.jpg
  #6  
Old December 4th 09, 03:01 AM posted to rec.aviation.homebuilt
cavelamb[_2_]
external usenet poster
 
Posts: 257
Default visualisation of the lift distribution over a wing

Alan Baker wrote:
In article ,
brian whatcott wrote:

Alan Baker wrote:
/snip/
Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.
That assertion is incorrect. You are no dummy so I'm sure you'll correct
it when you realize the errors.
Sorry, but it's not. Pressure is created by particle collisions.
Hmmm...looks like Jim expected too much from you: the kinetic theory of
gases has it that pressure may be computed from the temperature AND the
density of gases... that is to say, by retaining the SAME molar quantity
of gas, and raising its temperature (which translates to a higher
velocity), the pressure is increased P.V = R.t and all that....

Put it another way: each "hotter" molecule reverses direction at a
surface with greater force.

Brian W
I'm perfectly aware of that...

It took me too long to realise the problem: you have a problem with
saying: "Oh yes, I got it worng."


I didn't get anything wrong.

I am and was perfectly aware of the fact that the temperature of a gas
indicates a different average speed for the gas molecules and thus a
different momentum when the strike a surface.

People who WON'T do that in technical discussions qualify as people who
are just happy to stir up heated debate.


I agree. What of it.

I am going to leave this thread now: wrasslin' with pigs gets the
hands jest too soiled...


You can go.


I feel the same as Brian.
This had not been a discussion as much as a troll.

OF BLOODY COURSE, the high pressure area under the wing pushes up.
So what.

It couldn't possibly do that without the reduction of pressure on the top.
That's where all the magic is.

And you, sir, are a bloody bore.

So now, please also dismiss me.

  #7  
Old December 4th 09, 03:26 AM posted to rec.aviation.homebuilt
Alan Baker
external usenet poster
 
Posts: 244
Default visualisation of the lift distribution over a wing

In article ,
cavelamb wrote:

Alan Baker wrote:
In article ,
brian whatcott wrote:

Alan Baker wrote:
/snip/
Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.
That assertion is incorrect. You are no dummy so I'm sure you'll
correct
it when you realize the errors.
Sorry, but it's not. Pressure is created by particle collisions.
Hmmm...looks like Jim expected too much from you: the kinetic theory of
gases has it that pressure may be computed from the temperature AND the
density of gases... that is to say, by retaining the SAME molar quantity
of gas, and raising its temperature (which translates to a higher
velocity), the pressure is increased P.V = R.t and all that....

Put it another way: each "hotter" molecule reverses direction at a
surface with greater force.

Brian W
I'm perfectly aware of that...
It took me too long to realise the problem: you have a problem with
saying: "Oh yes, I got it worng."


I didn't get anything wrong.

I am and was perfectly aware of the fact that the temperature of a gas
indicates a different average speed for the gas molecules and thus a
different momentum when the strike a surface.

People who WON'T do that in technical discussions qualify as people who
are just happy to stir up heated debate.


I agree. What of it.

I am going to leave this thread now: wrasslin' with pigs gets the
hands jest too soiled...


You can go.


I feel the same as Brian.
This had not been a discussion as much as a troll.

OF BLOODY COURSE, the high pressure area under the wing pushes up.
So what.

It couldn't possibly do that without the reduction of pressure on the top.
That's where all the magic is.

And you, sir, are a bloody bore.

So now, please also dismiss me.


Look, I started out to clarify the point for those who have the wrong
perception of the situation...

....and it turned that there were such people.

I explicitly stated that if the OP meant that the low pressure above the
wing is responsible for two thirds of the pressure *difference* then he
was on solid ground (while allowing as how I didn't know what the
precise figures actually were).

Ever since then, types like you have been coming in and saying "IT
DOESN'T MATTER", when very clearly (because there are people who don't
understand the situation) it does.

It's like the downwash argument. You can say "IT DOESN'T MATTER", when
people argue that the air behind an aircraft is not deflected downward,
but it *does* matter. Having an accurate understanding of the physical
processes of flight matters.

--
Alan Baker
Vancouver, British Columbia
http://gallery.me.com/alangbaker/100008/DSCF0162/web.jpg
  #8  
Old December 4th 09, 10:13 PM posted to rec.aviation.homebuilt
Jim Logajan
external usenet poster
 
Posts: 1,958
Default visualisation of the lift distribution over a wing

Alan Baker wrote:
Jim Logajan wrote:
Alan Baker wrote:
Any change in pressure is *by definition* a change in the number of
particles in the fluid that are impacting the surface.


That assertion is incorrect. You are no dummy so I'm sure you'll
correct it when you realize the errors.


Sorry, but it's not. Pressure is created by particle collisions.


Brian Whatcott already addressed one of the errors I had in mind. The other
I had in mind was your incorrect assertion "*by definition*". You should
have asserted "*by derivation*". College level texts on statistical and
thermal physics *derive* the gas laws from statistical mechanics; they do
not present them as true "by definition." (Though that would make for short
textbooks!)
 




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