RE: Reflexed Airfoil and Flying Wings - Downwash?  
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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 3:58:04 PM   
Ben Lanterman



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Well anytime there is a dynamic process going on you can pretty well freeze it and do a force and moment diagram. We did that all the time before computers. Doing a dynamic analysis with a slide rule just gets you a smoky sliderule and another migraine headache.

Ok let us buy the assumption the air has to go down for the wing to go up. The only way that works is for there to be a transfer methodology involved. Air going down doesn't make the wing go up unless there are thousands of little force vectors pushing on the wing or maybe one big one. The CG of the wing must have a force on it. Right?

The Mv=mv and ma=ma is a great shorthand for eliminating the F inbetween. But indeed the F has to be there in one form or another. MwAw=Fw=Fdw=MdwAdw > mass wing x acc wing = force wing = force downwash = mass downwash acc downwash.

Rockets, guys throwing bricks on ice skates, etc. Sometime in that dynamic process is a force located for a time period and a change in mass. (The wing doesn't change mass so it makes it easier) Keeping it simple the force accelerates the brick as you throw it and the same force the opposite direction accelerates you because it is located in your palm. Similarly the pressure in the rocket chamber accelerates the exhaust one way and the rocket the other, etc.

There is a force interface in every condition you can suggest. We talk about it as if it weren't there, wing to go up requires air to go down, but we conveinently have forgotten to mention the force interface. But it is indeed there. Where there is motion there is force being applied. Right??

That means you must have a mechanism for the downwash to be converted into a force somewhere on the wing. In general the force wouldn't hard to find and normally the force is found where the CG is being accelerated. We have the wing being accelerated against 1g. We have the downwash being downward accelerated into the low pressure. So we have two masses being accelerated. Wing and downwash and we have corresponding forces.

Where is the force interface? The wing says the force on it is up at the 1/4 chord and is due to pressure. This is what all instruments that can be put on a wing's surface and their resultant measurements indicate (certainly close enought for government work most of the time).

Now - how does the downwash get the momentum, ma, etc. force to the wing? You must be able to find the force interface. Unless you can answer that - the downwash answer to lift is bogus.

If there is a big hand grabbing chunks of air and sweeping them downward you have the answer. It is the hand. If you are like the Harrier, it is the nozzles. It is very easy to recognize and find. Where is the interface when the wing is flinging the downwash down?

Just saying, "In order for the wing to stay up there, it has to send air down." isn't an answer. It must have a physical mechanism to resolve the forces involved. It isn't metaphysical or magic and angles are no longer carrying wings for us.

Any takers? Do you understand what I am asking?


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 4:41:19 PM   
KenLitko


 

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quote:

ORIGINAL: adam_one

After all those interesting observations it seems that you've missed an important detail:
In order for the wing to stay up there, it has to send air down.


Why? Why is that necessary. Prove it. This statement is nothing other than a hypothesis with no proof behind it.

Here is my proof...

The wing is sending air down, but it is also sending air up... The laws of physics say that in incompressible fluid dynamics... low speed aerodynamics... a.k.a. "the stuff that we are talking about"... it is physically impossible to shove part of a fluid down and create a force upward.

Why???

Easy... any parcel of fluid that is displaced downward MUST be replaced by a parcel of fluid that is displaced upward. The net effect is that there is no overall change in momentum of the fluid. With no change in momentum of the fluid, we cannot transfer any of it to the aircraft / wing / whatever.

So you ask... "Why can't we replace the downward moving parcel with another parcel of air from above?... then everything is moving downward"

That's exactly the trouble... then EVERYTHING is moving downwards... our little wing cannot produce enough force to move an infinite column of air downwards. It would have an infinite lifting force. And we would never be able to put enough thrust behind it to move even a little bit.

Ken - www.litkoaero.com

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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 5:00:50 PM   
KenLitko


 

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quote:

ORIGINAL: adam_one

One should not mix the wing tip vortices (vortex) with the wing's downwash.
Both occur at the same time due to the same pressure differences but at different locations where the tip vortices have negative effect on lift. The wing tip vortices are the price we pay for having lift as they create induced drag.


Not quite... wingtip votices do not cause induced drag.. they ARE induced drag. Wingtip votices are the price we pay for having a REAL wing. We would have more lift if we didn't have them.

We have upwash in front of a wing and downwash behind a wing if we do not have tip vortices. If we do have tip vortices, the upwash is decreased and the downwash is increased. **

** More downwash, less upwash... less lift.

All that happened was our lift vector got tilted backward... some of the lift is now pointing in the wrong direction... backward... and is now drag.

Ken - www.litkoaero.com


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 5:24:34 PM   
adam_one


 

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quote:

Why? Why is that necessary. Prove it. This statement is nothing other than a hypothesis with no proof behind it.
Lift occurs when a moving flow of gas is turned by a solid object. The flow is turned in one direction, and the lift is generated in the opposite direction, according to Newton's Third Law of action and reaction. Because air is a gas and the molecules are free to move about, any solid surface can deflect a flow. For an aircraft wing, both the upper and lower surfaces contribute to the flow turning.
You don't even need to take my word for it, the text above may be found in the following site:
http://www.grc.nasa.gov/WWW/K-12/airplane/lift1.html

quote:

Not quite... wingtip votices do not cause induced drag.. they ARE induced drag.
Not really, because the induced drag caused by the tip vortices may be reduced by drooped or raised wing tips, which forces the vortices further out.
So, you can't get rid of tip vortices but you can reduce their negative effect on lift by reducing the induced drag.

< Message edited by adam_one -- 3/21/2005 5:38:29 PM >


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 5:27:01 PM   
KenLitko


 

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quote:

ORIGINAL: Tim Green

BTW - here's a quote from NASA ...

"Lift occurs when a moving flow of gas is turned by a solid object. The flow is turned in one direction, and the lift is generated in the opposite direction, according to Newton's Third Law of action and reaction. Because air is a gas and the molecules are free to move about, any solid surface can deflect a flow. For an aircraft wing, both the upper and lower surfaces contribute to the flow turning. Neglecting the upper surface's part in turning the flow leads to an incorrect theory of lift."

You can find it here ...

http://www.grc.nasa.gov/WWW/K-12/airplane/lift1.html


That's correct.... from the freestream, turned up (upwash), turned over the airfoil, turned down (downwash) and turned back to the freestream (well mostly anyway... there is probably a lot of turbulence).

quote:

And an interesting book, by a couple of guys with plenty of credentials (yes - it's pro-newtonian - what else would I suggest?) ...

http://www.aa.washington.edu/faculty/eberhardt/lift.htm



I've read that a couple times and really didn't like it. Dr. Anderson and Eberhardt try to explain lift in the context of bad explanations and they give the reader "mental images" of lift without really explaining the true mechanism, which is quite complex.

Ken - www.litkoaero.com

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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 5:49:36 PM   
KenLitko


 

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quote:

ORIGINAL: adam_one

Lift occurs when a moving flow of gas is turned by a solid object. The flow is turned in one direction, and the lift is generated in the opposite direction, according to Newton's Third Law of action and reaction. Because air is a gas and the molecules are free to move about, any solid surface can deflect a flow. For an aircraft wing, both the upper and lower surfaces contribute to the flow turning.

You don't even need to take my word for it, the text above may be found in the following site:
http://www.grc.nasa.gov/WWW/K-12/airplane/lift1.html


adam_one,

The above site says that the flow is turned, not "sent down". Turning something and shoving it in one direction are two different things.

"Turned flow" = circulation

The air is turned AROUND the wing; the wing doesn't turn it and push it in one direction or another.

quote:

ORIGINAL: KenLitko

Not quite... wingtip votices do not cause induced drag.. they ARE induced drag.


quote:

ORIGINAL: adam_one
Not really, because the induced drag caused by tip vortices may be reduced by drooped or raised wing tips, which forces the vortices further out.
So, you can't get rid of tip vortices but you can reduce their negative effect on lift by reducing the induced drag.


Moving the wingtip vortices further out alters their strength... reduced strength = reduced downwash = more lift.

Ken - www.litkoaero.com

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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 5:53:20 PM   
adam_one


 

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It is stated:
The flow is turned in one direction, and the lift is generated in the opposite direction.
Which is the opposite direction of lift?

Come'on you're pulling my leg.

quote:

Moving the wingtip vortices further out alters their strength... reduced strength = reduced downwash = more lift.

Anyway, the wing tip vortices are not induced drag, they are just wing tip vortices.
And the downwash at the wing tip vortices do not create lift.
Lift is created by the downwash observed at the wings TE.

< Message edited by adam_one -- 3/21/2005 6:38:15 PM >


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 6:37:56 PM   
KenLitko


 

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quote:

ORIGINAL: adam_one

It is stated:
The flow is turned in one direction, and the lift is generated in the opposite direction.
Which is the opposite direction of lift?


Looking at a wing from the tip, inboard... with the windward edge at the left, the flow is turned in the _clockwise_ direction.

The NASA web pages degenerate into a "net downward momentum lifts wing up" explanation even though they try not to.

You would impress me if you could show me that you could create a net downward momentum of air in a 3D world using an incompressible fluid.

Ken - www.litkoaero.com



< Message edited by KenLitko -- 3/21/2005 6:40:58 PM >


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 6:45:32 PM   
adam_one


 

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quote:

The NASA web pages degenerate into a F=ma explanation even though they try not to.

Wow, so NASA is not totally right, well, well, well...

The picture below shows how the whole downwash rotates viewed from the front.


Attachments
Click to see fullsize image.
Click for fullsize


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 6:45:58 PM   
KenLitko


 

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quote:

ORIGINAL: adam_one
...
Anyway, the wing tip vortices are not induced drag, they are just wing tip vortices.
And the downwash at the wing tip vortices do not create lift.
Lift is created by the downwash observed at the wings TE.


So, the "trailing edge downwash" and the "wing tip vortex downwash" lead to two different types of downward momentum..... One that carries momentum and creates lift... and one that just whistles on by.

Come on... who's pulling who's leg?

So where is our source of induced drag?

All of these things are interrelated...

Ken - www.litkoaero.com

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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 6:50:56 PM   
KenLitko


 

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quote:

ORIGINAL: adam_one

quote:

The NASA web pages degenerate into a F=ma explanation even though they try not to.

Wow, so NASA is not totally right, well, well, well...

The picture below shows how the whole downwash rotates viewed from the front.



Yeah yeah yeah... :-)

BTW... I corrected the "F=ma"... which still applies, but replaced it with the "downward momentum thingy" :-)

Back to our regularly scheduled program...

OK... nice picture... what is happening on the top of the wing? Where is that air coming from?

Ken - www.litkoaero.com

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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 7:03:33 PM   
adam_one


 

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Look at the picture below, almost everything is shown there:

Attachments
Click to see fullsize image.
Click for fullsize


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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 7:12:56 PM   
KenLitko


 

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How does that contradict what I am saying? It appears to have a very strong upturn at the end of the sheet, outboard of the wing... judging by the size of the flow indicator.

Are you telling me that in subsonic flow the only air that matters is the air that is directly behind and underneath the wing after the wing has passed? Nothing in front of the wing or outboard of the wingtip matters?

Ken - www.litkoaero.com

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RE: Reflexed Airfoil and Flying Wings - Downwash? - 3/21/2005 7:23:02 PM   
Ben Lanterman



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"]Lift occurs when a moving flow of gas is turned by a solid object. The flow is turned in one direction, and the lift is generated in the opposite direction, according to Newton's Third Law of action and reaction. Because air is a gas and the molecules are free to move about, any solid surface can deflect a flow. For an aircraft wing, both the upper and lower surfaces contribute to the flow turning."

Where is the force interface between the downwash and the wing? You are sideslipping the real question. How does the flow turning make force on the wing?