On Wed, 7 Dec 2005, Rick Monteverde wrote:

> >But the incoming air will fill the vacuum chamber, with
> >the wave travelling at roughly the speed of sound!
> >In human time scale, as soon as you open the valve
> >and generate an air jet, significant air pressure
> >appears on the OTHER side of the wing.  You can't
> >just claim that the pressure there is insignificant,
> >instead you have to measure it, millisecond by millisecond.
>
> The pump is large compared to the small jar volume, and once that dense
> air in the jet disperses, which it does very quickly, density and
> pressure get pretty low pretty fast before much of it swirls around
> underneath the foil. To see it and its scale is convincing. Seeing my
> writing about it isn't.

Eh.   Seeing the demonstration wouldn't convince me, since my brain would
insist that "SINCE the airfoil is deflected upwards, THEREFORE the
pressure underneath is greater than the pressure above."

:)

>
> >If you can show that air can PULL on a curved wing
> >(i.e. create an absolute negative pressure,)
> >that's something very interesting.
>
> Yup. It's been shown too, but not by me. Google should bring it up with
> words like van der Waals, airfoil, boundary layer, etc.

But that's just lowered pressure, not absolute negative (attraction)
pressure.

Boundary layer stuff is weird, but I've never seen articles talking about
negative gas pressure.

It's hard to see how a molecule, by colliding with a surface, could
*attract* that surface.  And it's hard to see how widely separated
molecules could attract each other on average, especially if they're
moving fast enough to bounce during collisions (which would create a
strong repulsion force which would have to be canceled out by any
attraction mechanism.)  If they don't bounce during collisions, then
that's called condensation.   :)

> Why else would a
> flow stick against a surface and follow it down around a curve like
> that?

For air jets in air, or for water jets underwater, Coanda Effect explains
it:  air flows always entrain adjacent air, pulling the adjacent air into
the flow.  Or said another way, flows always represent lower pressure, so
if air is flowing parallel to an object, the perpendicular force between
the flow and the object will be reduced, causing the flow and the object
to accelerate towards each other as the outer (non-flowing) air exerts its
non-reduced pressure.  Blow some air parallel to one side of a dangling
piece of paper and the paper will be pushed into the flow so it "adheres"
to the flow.  And the flow will "stick" to the paper, bending away from
it's original trajectory.


Separate topic: In that old SciAm article about Coanda Effect, they found
that tiny structures within the boundary layer could have large effects,
so a small step or striation on the surface would make the flow-adhesion
effect stronger.  I remember one oddity from conventional textbooks: if
you put a polished sphere in a wind tunnel, the smoke will curve around
the sphere and follow the back of the sphere for quite a ways before
"detaching" and becoming turbulent... but if you add a small disk of thin
sandpaper (or even roughened paint) to the very front of the sphere, the
smoke then detaches right at the circumference of the sphere, and it won't
follow the curve around to the back of the sphere at all.  Just that tiny
change to the front of the sphere will put the entire rear of the sphere
into "stall mode."

Aircraft designers know all about the effect:  just a small bit of rough
ice on the leading edge and top of an aircraft wing will trigger early
flow-detachment, ruining the lift and leading to crashes on takeoff.
That's why they're so paranoid about "de-icing" the tops of airliner
wings.  The airfoil bottoms are mostly irrelevant (and you can even hang
huge fuel tanks and racks of missles down there.)

Also there's a whole group of experimental aircraft hobbyists who
specialize in high-lift "laminar flow" wings with highly polished upper
surfaces.  These aren't widely used because their characteristics are
seriously altered by a small bit of raindrops clinging to the wing.


>
> I never finished construction on it, but I started a rig where the
> airfoil sat on a membrane with good vacuum under the membrane in a
> separate chamnber from the air above the foil. Air jet would hit the top
> of the foil as before, but the whole bottom side would be against the
> membrane. Pump would keep the air above at as low a pressure as possible
> while the jet shot across the foil surface.

Now THAT would be more convincing (even more convincing that measuring the
pressure under your first airfoil.)

> I figure the foil would
> still rise into the airflow, pulling up on the membrane with the
> certain-to-be-lower pressure below it.
>
> Maybe simpler to use a split chamber with water instead of air?

Or use an oil stream in a vacuum?   But then you might get genuinely
negative fluid pressure, the same negative pressure that's the source of
"surface tension."



>
> - Rick
>
>
>
>

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