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Airplane Pilot's As Physicists



 
 
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  #1  
Old October 25th 07, 06:56 PM posted to sci.physics,rec.aviation.piloting
Bertie the Bunyip[_19_]
external usenet poster
 
Posts: 3,851
Default Airplane Pilot's As Physicists

jon wrote in news:1193334432.867133.306890
@t8g2000prg.googlegroups.com:

http://www.efluids.com/efluids/galle...s/Morris_3.jsp


And what's that mysterios fuzz on the top of the wings, fjukkwit?



Bertie
  #2  
Old October 16th 07, 07:41 PM posted to sci.physics,rec.aviation.piloting
Jim Logajan
external usenet poster
 
Posts: 1,958
Default Airplane Pilot's As Physicists

Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htm and
http://www.physicsmyths.org.uk/drag.htm for a closer examination of
the physics behind the aerodynamic lift and drag.


You might want to actually _include_ Bernoulli's theorem somewhere in your
pages. You talk about Bernoulli's equation, Bernoulli's principle, and
Bernoulli's law. And yet none of them are actually presented. Are you
saying they all the same or all different? Why not use the terminology used
by the professionals and stick with "Bernoulli's theorem"? How about
including references to relevant texts on your pages? It's not like serious
texts and lab experiments haven't been done on the subject for a zillion
years. It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and done your
own relevant research.

You might also want to redraw your figures so they include vertical labeled
arrows. Then present the assumptions and math needed to show your work and
why you think the vertical magnitudes sum to zero. Just saying they do, or
they only yield a torque, isn't good enough. It is more useful to _show_ -
not pontificate and hand-wave.

P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on Physics is
as good a place as any to start.
  #3  
Old October 16th 07, 09:31 PM posted to sci.physics,rec.aviation.piloting
Thomas
external usenet poster
 
Posts: 6
Default Airplane Pilot's As Physicists

On 16 Oct, 19:41, Jim Logajan wrote:
Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htm for a closer examination of
the physics behind the aerodynamic lift and drag.


You might want to actually _include_ Bernoulli's theorem somewhere in your
pages. You talk about Bernoulli's equation, Bernoulli's principle, and
Bernoulli's law. And yet none of them are actually presented. Are you
saying they all the same or all different? Why not use the terminology used
by the professionals and stick with "Bernoulli's theorem"? How about
including references to relevant texts on your pages? It's not like serious
texts and lab experiments haven't been done on the subject for a zillion
years. It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and done your
own relevant research.

You might also want to redraw your figures so they include vertical labeled
arrows. Then present the assumptions and math needed to show your work and
why you think the vertical magnitudes sum to zero. Just saying they do, or
they only yield a torque, isn't good enough. It is more useful to _show_ -
not pontificate and hand-wave.

P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on Physics is
as good a place as any to start.


Bernoulli's theorem is not a fundamental physical law and thus not
required to understand the principle behind the aerodynamic lift. And
its misinterpretation and misapplication quite evidently leads to
incorrect physical conclusions, like the claim that a moving gas would
inherently have a lower static pressure than a stationary one. The net
flow velocity of a gas has per se nothing to do with the static
pressure.
As a thought experiment, consider a large tank containing gas with a
pipe attached to it which leads into a vacuum space. Assume first this
pipe is closed at the end; then the flow velocity in the pipe is zero
because the molecules heading outwards will be reflected at the end
and reverse their velocity (assume for simplicity that the molecules
do not collide with each other but only with the walls of the pipe and
the tank). If one now opens the pipe, the only thing that changes is
that the molecules heading outwards will not be reflected anymore at
the end but simply carry on heading into the vacuum space (with the
corresponding loss of molecules being replaced from the large tank).
So we now have a net flow velocity within the pipe without that either
the density nor the speed of the molecules has changed in any way.
This means that the pressure exerted on the inside wall of the pipe is
unchanged despite the fact that we now have a net flow velocity within
it. So Bernoulli's theorem would quite evidently give a wrong result
here.

Thomas


  #4  
Old October 17th 07, 12:48 AM posted to sci.physics,rec.aviation.piloting
Le Chaud Lapin
external usenet poster
 
Posts: 291
Default Airplane Pilot's As Physicists

On Oct 16, 3:31 pm, Thomas wrote:
On 16 Oct, 19:41, Jim Logajan wrote:





Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htmfor a closer examination of
the physics behind the aerodynamic lift and drag.


You might want to actually _include_ Bernoulli's theorem somewhere in your
pages. You talk about Bernoulli's equation, Bernoulli's principle, and
Bernoulli's law. And yet none of them are actually presented. Are you
saying they all the same or all different? Why not use the terminology used
by the professionals and stick with "Bernoulli's theorem"? How about
including references to relevant texts on your pages? It's not like serious
texts and lab experiments haven't been done on the subject for a zillion
years. It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and done your
own relevant research.


You might also want to redraw your figures so they include vertical labeled
arrows. Then present the assumptions and math needed to show your work and
why you think the vertical magnitudes sum to zero. Just saying they do, or
they only yield a torque, isn't good enough. It is more useful to _show_ -
not pontificate and hand-wave.


P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on Physics is
as good a place as any to start.


Bernoulli's theorem is not a fundamental physical law and thus not
required to understand the principle behind the aerodynamic lift. And
its misinterpretation and misapplication quite evidently leads to
incorrect physical conclusions, like the claim that a moving gas would
inherently have a lower static pressure than a stationary one. The net
flow velocity of a gas has per se nothing to do with the static
pressure.


I so agree. The amout of hand-waving that goes on when (presumably
technically-inclined) individuals invoke Bernoulli is perplexing.
Oddly, my college physics book is almost as guilty - after chapters
and chapters of Newtonian mechanics that are quite clear, they seem to
imply just that.

As a thought experiment, consider a large tank containing gas with a
pipe attached to it which leads into a vacuum space. Assume first this
pipe is closed at the end; then the flow velocity in the pipe is zero
because the molecules heading outwards will be reflected at the end
and reverse their velocity (assume for simplicity that the molecules
do not collide with each other but only with the walls of the pipe and
the tank). If one now opens the pipe, the only thing that changes is
that the molecules heading outwards will not be reflected anymore at
the end but simply carry on heading into the vacuum space (with the
corresponding loss of molecules being replaced from the large tank).
So we now have a net flow velocity within the pipe without that either
the density nor the speed of the molecules has changed in any way.
This means that the pressure exerted on the inside wall of the pipe is
unchanged despite the fact that we now have a net flow velocity within
it. So Bernoulli's theorem would quite evidently give a wrong result
here.


Hmmm...technically, someone could argue that, in the vicinity of the
exit hole of the tank, there would be resulting decrease in pressure,
which would be true.

The misapplication, I think, results from too much hand-waving and not
being very specific about what pressure decreases over what. A venturi
apparutus, for example, very clearly demonstrates a drop in pressure,
and that drop is real, but the points chosen to measure the pressure
in the apparutus is very specific.

-Le Chaud Lapin-

  #5  
Old October 17th 07, 01:57 AM posted to sci.physics,rec.aviation.piloting
Bertie the Bunyip[_19_]
external usenet poster
 
Posts: 3,851
Default Airplane Pilot's As Physicists

Le Chaud Lapin wrote in
oups.com:

On Oct 16, 3:31 pm, Thomas wrote:
On 16 Oct, 19:41, Jim Logajan wrote:





Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htmfor a closer examination of
the physics behind the aerodynamic lift and drag.


You might want to actually _include_ Bernoulli's theorem somewhere
in your pages. You talk about Bernoulli's equation, Bernoulli's
principle, and Bernoulli's law. And yet none of them are actually
presented. Are you saying they all the same or all different? Why
not use the terminology used by the professionals and stick with
"Bernoulli's theorem"? How about including references to relevant
texts on your pages? It's not like serious texts and lab
experiments haven't been done on the subject for a zillion years.
It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and
done your own relevant research.


You might also want to redraw your figures so they include vertical
labeled arrows. Then present the assumptions and math needed to
show your work and why you think the vertical magnitudes sum to
zero. Just saying they do, or they only yield a torque, isn't good
enough. It is more useful to _show_ - not pontificate and
hand-wave.


P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on
Physics is as good a place as any to start.


Bernoulli's theorem is not a fundamental physical law and thus not
required to understand the principle behind the aerodynamic lift. And
its misinterpretation and misapplication quite evidently leads to
incorrect physical conclusions, like the claim that a moving gas
would inherently have a lower static pressure than a stationary one.
The net flow velocity of a gas has per se nothing to do with the
static pressure.


I so agree. The amout of hand-waving that goes on when (presumably
technically-inclined) individuals invoke Bernoulli is perplexing.
Oddly, my college physics book is almost as guilty - after chapters
and chapters of Newtonian mechanics that are quite clear, they seem to
imply just that.

As a thought experiment, consider a large tank containing gas with a
pipe attached to it which leads into a vacuum space. Assume first
this pipe is closed at the end; then the flow velocity in the pipe is
zero because the molecules heading outwards will be reflected at the
end and reverse their velocity (assume for simplicity that the
molecules do not collide with each other but only with the walls of
the pipe and the tank). If one now opens the pipe, the only thing
that changes is that the molecules heading outwards will not be
reflected anymore at the end but simply carry on heading into the
vacuum space (with the corresponding loss of molecules being replaced
from the large tank). So we now have a net flow velocity within the
pipe without that either the density nor the speed of the molecules
has changed in any way. This means that the pressure exerted on the
inside wall of the pipe is unchanged despite the fact that we now
have a net flow velocity within it. So Bernoulli's theorem would
quite evidently give a wrong result here.


Hmmm...technically, someone could argue that, in the vicinity of the
exit hole of the tank, there would be resulting decrease in pressure,
which would be true.

The misapplication, I think, results from too much hand-waving and not
being very specific about what pressure decreases over what. A venturi
apparutus, for example, very clearly demonstrates a drop in pressure,
and that drop is real, but the points chosen to measure the pressure
in the apparutus is very specific.


Hey, i'm waving my hand!

Well, just one finger, to be precise..


Bertie
  #6  
Old October 17th 07, 09:41 AM posted to sci.physics,rec.aviation.piloting
Thomas
external usenet poster
 
Posts: 6
Default Airplane Pilot's As Physicists

On 17 Oct, 00:48, Le Chaud Lapin wrote:
On Oct 16, 3:31 pm, Thomas wrote:



On 16 Oct, 19:41, Jim Logajan wrote:


Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htmfora closer examination of
the physics behind the aerodynamic lift and drag.


You might want to actually _include_ Bernoulli's theorem somewhere in your
pages. You talk about Bernoulli's equation, Bernoulli's principle, and
Bernoulli's law. And yet none of them are actually presented. Are you
saying they all the same or all different? Why not use the terminology used
by the professionals and stick with "Bernoulli's theorem"? How about
including references to relevant texts on your pages? It's not like serious
texts and lab experiments haven't been done on the subject for a zillion
years. It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and done your
own relevant research.


You might also want to redraw your figures so they include vertical labeled
arrows. Then present the assumptions and math needed to show your work and
why you think the vertical magnitudes sum to zero. Just saying they do, or
they only yield a torque, isn't good enough. It is more useful to _show_ -
not pontificate and hand-wave.


P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on Physics is
as good a place as any to start.


Bernoulli's theorem is not a fundamental physical law and thus not
required to understand the principle behind the aerodynamic lift. And
its misinterpretation and misapplication quite evidently leads to
incorrect physical conclusions, like the claim that a moving gas would
inherently have a lower static pressure than a stationary one. The net
flow velocity of a gas has per se nothing to do with the static
pressure.


I so agree. The amout of hand-waving that goes on when (presumably
technically-inclined) individuals invoke Bernoulli is perplexing.
Oddly, my college physics book is almost as guilty - after chapters
and chapters of Newtonian mechanics that are quite clear, they seem to
imply just that.


It is not so much a case of 'hand waving' arguments, but of
insufficient and contradictory physical definitions (especially with
regard to the notion of an 'inviscid' gas). Applying some physical
equation to a situation where it can not be applied is bound to lead
to paradoxes and wrong results.




As a thought experiment, consider a large tank containing gas with a
pipe attached to it which leads into a vacuum space. Assume first this
pipe is closed at the end; then the flow velocity in the pipe is zero
because the molecules heading outwards will be reflected at the end
and reverse their velocity (assume for simplicity that the molecules
do not collide with each other but only with the walls of the pipe and
the tank). If one now opens the pipe, the only thing that changes is
that the molecules heading outwards will not be reflected anymore at
the end but simply carry on heading into the vacuum space (with the
corresponding loss of molecules being replaced from the large tank).
So we now have a net flow velocity within the pipe without that either
the density nor the speed of the molecules has changed in any way.
This means that the pressure exerted on the inside wall of the pipe is
unchanged despite the fact that we now have a net flow velocity within
it. So Bernoulli's theorem would quite evidently give a wrong result
here.


Hmmm...technically, someone could argue that, in the vicinity of the
exit hole of the tank, there would be resulting decrease in pressure,
which would be true.


As should be evident from what I said above already, for an inviscid
gas (i.e. assuming the molecules do not collide with each other but
only with the walls), it should not make any difference whatsoever if
the pipe is open or closed at the end. The rate with which the
molecules hit the inside wall (and thus the pressure on it) is exactly
the same anywhere within the pipe (assuming the lost molecules for the
open pipe situation are readily replaced from the tank).


The misapplication, I think, results from too much hand-waving and not
being very specific about what pressure decreases over what. A venturi
apparutus, for example, very clearly demonstrates a drop in pressure,
and that drop is real, but the points chosen to measure the pressure
in the apparutus is very specific.


The Venturi effect (like the paper sheet example, the Coanda effect
and the Magnus effect) is merely a result of the viscosity of the
medium. It does not occur for an ideally inviscid medium (i.e. if the
collisions of molecules amongst each other can be neglected), whereas
the aerodynamic lift does.

Thomas



  #7  
Old October 25th 07, 07:18 PM posted to sci.physics,rec.aviation.piloting
jon
external usenet poster
 
Posts: 8
Default Airplane Pilot's As Physicists

On 17 Okt, 01:48, Le Chaud Lapin wrote:
On Oct 16, 3:31 pm, Thomas wrote:





On 16 Oct, 19:41, Jim Logajan wrote:


Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htmfora closer examination of
the physics behind the aerodynamicliftand drag.


You might want to actually _include_Bernoulli'stheorem somewhere in your
pages. You talk aboutBernoulli'sequation,Bernoulli'sprinciple, and
Bernoulli'slaw. And yet none of them are actually presented. Are you
saying they all the same or all different? Why not use the terminology used
by the professionals and stick with "Bernoulli'stheorem"? How about
including references to relevant texts on your pages? It's not like serious
texts and lab experiments haven't been done on the subject for a zillion
years. It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and done your
own relevant research.


You might also want to redraw your figures so they include vertical labeled
arrows. Then present the assumptions and math needed to show your work and
why you think the vertical magnitudes sum to zero. Just saying they do, or
they only yield a torque, isn't good enough. It is more useful to _show_ -
not pontificate and hand-wave.


P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on Physics is
as good a place as any to start.


Bernoulli'stheorem is not a fundamental physical law and thus not
required to understand the principle behind the aerodynamiclift. And
its misinterpretation and misapplication quite evidently leads to
incorrect physical conclusions, like the claim that a moving gas would
inherently have a lower static pressure than a stationary one. The net
flow velocity of a gas has per se nothing to do with the static
pressure.


I so agree. The amout of hand-waving that goes on when (presumably
technically-inclined) individuals invokeBernoulliis perplexing.
Oddly, my college physics book is almost as guilty - after chapters
and chapters of Newtonian mechanics that are quite clear, they seem to
imply just that.





As a thought experiment, consider a large tank containing gas with a
pipe attached to it which leads into a vacuum space. Assume first this
pipe is closed at the end; then the flow velocity in the pipe is zero
because the molecules heading outwards will be reflected at the end
and reverse their velocity (assume for simplicity that the molecules
do not collide with each other but only with the walls of the pipe and
the tank). If one now opens the pipe, the only thing that changes is
that the molecules heading outwards will not be reflected anymore at
the end but simply carry on heading into the vacuum space (with the
corresponding loss of molecules being replaced from the large tank).
So we now have a net flow velocity within the pipe without that either
the density nor the speed of the molecules has changed in any way.
This means that the pressure exerted on the inside wall of the pipe is
unchanged despite the fact that we now have a net flow velocity within
it. SoBernoulli'stheorem would quite evidently give a wrong result
here.


Hmmm...technically, someone could argue that, in the vicinity of the
exit hole of the tank, there would be resulting decrease in pressure,
which would be true.

The misapplication, I think, results from too much hand-waving and not
being very specific about what pressure decreases over what. A venturi
apparutus, for example, very clearly demonstrates a drop in pressure,
and that drop is real, but the points chosen to measure the pressure
in the apparutus is very specific.

-Le Chaud Lapin-- Dölj citerad text -

- Visa citerad text -- Dölj citerad text -

- Visa citerad text -


The venturi pipe is mostly misunderstood. To get through the narrow
section, the fluid must be pressed against the convergent part with a
higher pressure. The Coanda effect forces the fluid to follow the
walls in the divergent part.

All early speed sensors in 1920 used only the divergent part of the
venturi pipe.

Look att Bleriot and other planes. Look at Piper Colt 1953 model with
its backpart venturi. The front convergent part was not needed.

Changing the airflow direction over and under the wing, creates the
local pressure gradients + or - .

  #8  
Old October 25th 07, 07:08 PM posted to sci.physics,rec.aviation.piloting
jon
external usenet poster
 
Posts: 8
Default Airplane Pilot's As Physicists

On 16 Okt, 20:41, Jim Logajan wrote:
Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htm for a closer examination of
the physics behind the aerodynamicliftand drag.


You might want to actually _include_Bernoulli'stheorem somewhere in your
pages. You talk aboutBernoulli'sequation,Bernoulli'sprinciple, andBernoulli'slaw. And yet none of them are actually presented. Are you
saying they all the same or all different? Why not use the terminology used
by the professionals and stick with "Bernoulli'stheorem"? How about
including references to relevant texts on your pages? It's not like serious
texts and lab experiments haven't been done on the subject for a zillion
years. It helps to show you know what you're talking about by showing
you've first read the professional literature on the subject and done your
own relevant research.

You might also want to redraw your figures so they include vertical labeled
arrows. Then present the assumptions and math needed to show your work and
why you think the vertical magnitudes sum to zero. Just saying they do, or
they only yield a torque, isn't good enough. It is more useful to _show_ -
not pontificate and hand-wave.

P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on Physics is
as good a place as any to start.



Nobelprizewinner Feynman made a good statement about the fluid
Bernoulli equation was valid for, "ideal fluid".

Feynman called the perfect fluid for "dry water" and it did not
exsist i a real world, only the mathematical world.

  #9  
Old October 26th 07, 07:21 AM posted to sci.physics,rec.aviation.piloting
Bertie the Bunyip[_19_]
external usenet poster
 
Posts: 3,851
Default Airplane Pilot's As Physicists

jon wrote in
oups.com:

On 16 Okt, 20:41, Jim Logajan wrote:
Thomas wrote:
You may want to check out my web pages
http://www.physicsmyths.org.uk/bernoulli.htmand
http://www.physicsmyths.org.uk/drag.htm for a closer examination of
the physics behind the aerodynamicliftand drag.


You might want to actually _include_Bernoulli'stheorem somewhere in
your pages. You talk aboutBernoulli'sequation,Bernoulli'sprinciple,
andBernoulli'slaw. And yet none of them are actually presented. Are
you saying they all the same or all different? Why not use the
terminology used by the professionals and stick with
"Bernoulli'stheorem"? How about including references to relevant
texts on your pages? It's not like serious texts and lab experiments
haven't been done on the subject for a zillion years. It helps to
show you know what you're talking about by showing you've first read
the professional literature on the subject and done your own relevant
research.

You might also want to redraw your figures so they include vertical
labeled arrows. Then present the assumptions and math needed to show
your work and why you think the vertical magnitudes sum to zero. Just
saying they do, or they only yield a torque, isn't good enough. It is
more useful to _show_ - not pontificate and hand-wave.

P.S. Chapter section 40-3 in volume 2 of Feynman's Lectures on
Physics is as good a place as any to start.



Nobelprizewinner Feynman made a good statement about the fluid
Bernoulli equation was valid for, "ideal fluid".

Feynman called the perfect fluid for "dry water" and it did not
exsist i a real world, only the mathematical world.



You're an idiot.


Bertie
 




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