RE: Jef Raskin article on aerodynamics in Fly RC Magazine  
View related threads: (in this forum | in all forums)

Tower Hobbies
Enter up to 4 keywords or Tower stock numbers
Logged in as Guest



Users viewing this topic: none
  Printable Version
       

All Forums >> RC Airplanes >> Aerodynamics >> RE: Jef Raskin article on aerodynamics in Fly RC Magazine
Page: <<   < prev  1 2 3 [4] 5 6 7 8 9   next >   >>  

Login
Message << Older Topic   Newer Topic >>
RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 5:36:48 AM   
Gremlin Castle


 

Posts: 1220
Joined: 2/9/2004
From: Arlington, TX, USA
Status: offline
I have been following the thread with interest and find that almost every topic in here has been covered by By Dr. Michael Selig and his group over the last 20 years.
For those that are dismissive of titled people, you should know that Selig started as a modeler and carried his interests on to study and create airfoils that are purpose designed for models. He also designed the wing for the NASA Helios project. The Span is in excess of 300 ft. On the other end of the spectrum his airfoil research has found application in the DARPA micro uavs.
His body of work is easily accessed by using any search engine which will take you to dozens of links featuring his work.
How do I know he started as a modeler? His mother would bring him over to the house when he was too young to drive so that I could help him with his models.

_____________________________

Up elevator is not always your friend.

(in reply to Ben Lanterman)
       Post #: 76

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 2:08:47 PM   
Ben Lanterman



Posts: 1284
Joined: 10/27/2002
From: St. Charles, MO, USA
Status: offline
I am a real fan of Dr. Michael's work. I am also jealous that he got the mind that could handle the math and I didn't. My son Aaron also got one of those minds and is a Dr. in EE specializing in radar at Georgia Tech. I really enjoy talking to those kind of guys.

leszek_k - you are wrong because you are missing the fundamentals in how mv rocket = mv exhaust came about.

It is just a mathematical result. Here is how it works.

Rocketmass x Rocket acceleration = Rocketforce. Where Rocketforce is the force applied to the Rocket center of gravity.

Exhaustgasmass x Exhaustgasacceleration = Exhasustgasforce. Where Exhaustgasforce is the force applied to the Exhaust gas.

Temperature of combustion determines the pressure force on the Exhaustgas. Remember all the old rockets that blew up. Pressure of combuston.

The location of the pressures in the rocket and compustion chamber, lets use a modern one where we mix the fuels just forward of the nozzle so max burning and pressure is in the nozzle.

Shorten the stuff - Rm x Ra = Rf and Em x Ea = Ef

Right at the surface of the nozzle and those areas Rf = Ef

So you can say Rm x Ra = Em x Ea

Integrate over time (V = integral a dt )and you get Rm x Rv = Em x Ev

Which is what you were trying to describe. The rocket does indeed work on the pressure principle..... we say it is reaction but reaction is a shorthand way of saying what happened in the equations above. It gets boring as all heck to have to say all that stuff each time we want to describe a rocket in the air so rational men agreed to bypass it and get to the end and call it reaction. Ion reaction works the same way. You expel an ion out the back. The mass and acceleration of the ion gives you a force that is going to be useful up to near the speed of light.

Mother nature loves everything in balance - The pressure force that is pushing the downwash air down is the gravity force trying to pull the air down into the vacuum. The pressure force that is caused by gravity is pushing the wing up is reacted by the wing. Mother nature abhors a vacuum - ever hear of that? The air above rushed in and the air below would do the same but the wing is in the way so the air below pushes the wing up in front of it.

leszek_k - go back and study your physics, you have it wrong. I had a course in rockets while in college :-) Hated it but got the fundamentals.


_____________________________

Ben Lanterman

(in reply to leszek_k)
       Post #: 77

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 3:02:34 PM   
LouW



Posts: 804
Joined: 1/1/2003
From: Moreland, GA, USA
Status: offline
There are two ways of looking at rocket propulsion also. Almost everyone understands that the reaction to an ejected mass is what pushes the rocket. In the case of the rocket, it is relatively easy to measure the mass ejected, the velocity with which it is expelled thus do the calculations for design. On the other hand, if you consider the actual forces acting in the combustion chamber, you will discover the mechanism through which the force is applied. The same pressure that accelerates the ejected mass is also exerted against the chamber walls. The summation of pressures in the forward direction is the way the reaction force is applied. However measuring and integrating this force is not easy and is usually not considered as a major design activity. (Of course designing for the high chamber pressures are important, it’s just that they aren’t required to define propulsive force.)

It is a little curious that engineers tend to look at only part of a system (the part that is easy to measure and calculate) and ignore (sometimes even deny the existence of) the remainder. An inviscid fluid can only exert a force by differential pressure. However, such differential pressure can only exist if there is an acceleration of a mass of fluid. By definition a fluid has a zero stress strain relationship, and if it’s inviscid, shear forces are zero. The only remaining mechanism by which a difference in pressure can be created is the acceleration of a mass of the fluid.

As a wing moves at an angle through the air, the air above tries to move into the space vacated above the wing, however since it has mass, it doesn’t move instantaneously, but is accelerated toward the space. Two things happen. An area of reduced pressure is formed above the wing (Boyle’s law), and the affected mass of air acquires a downward motion. These things must happen together. The actions are inseparable. They are essential parts of the same action. One simply can’t exist without the other. One is not merely the by-product of the other but they are both necessary parts of the whole.

The fact that engineers tend to deal with the part that is easier to measure and calculate, and ignore the rest, doesn’t make the rest any less true.

Without the deflection (acceleration) of air there can be no pressure field developed therefore no lift. It’s really that simple.

(in reply to leszek_k)
       Post #: 78

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 3:55:39 PM   
leszek_k


 

Posts: 30
Joined: 7/25/2003
From: Dubai, UNITED ARAB EMIRATES
Status: offline
Ben wrote :

>Rocketmass x Rocket acceleration = Rocketforce. Where Rocketforce is the force applied to the Rocket center of gravity.
>Exhaustgasmass x Exhaustgasacceleration = Exhasustgasforce. Where Exhaustgasforce is the force applied to the Exhaust gas.

I wrote :

>... rocket engine ...... expells a mass of gas with certain velocity to create a reaction called (in this case) thrust

Isn't it the same Ben - trust accelerates a rocket, and I though it was obvious that if a gas has to have some velocity it has to be accelerated first. Sorry for a shortcut. BTW, I have heard about one guy called Newton too, also something like F=m*a - what was it all about ?

Ben wrote :

>Temperature of combustion determines the pressure force on the Exhaustgas. Remember all the old rockets that blew up. Pressure of >combuston.

You should know better than that. It does not. In classic rocket engine pressure is determined by an amount of fuel burnt in given time - again I took a shortcut.
Again - remember ion engines. And no pressusre in a chamber - actually no chamber at all.

Talking about a pressure in a combustion chamber being source of trust, I think Mr Pascal would disagree with you.

Anyway, I think this discussion got quite hot, and not constructive at all.

Our planes will fly no matter who is guilty - Bernoulli or Newton.
Just moved to a new house so need to setup my workshop - and this is my priority now.

Have fun guys, safe landings.

< Message edited by leszek_k -- 2/17/2005 5:57:59 PM >

(in reply to Ben Lanterman)
       Post #: 79

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 4:02:37 PM   
leszek_k


 

Posts: 30
Joined: 7/25/2003
From: Dubai, UNITED ARAB EMIRATES
Status: offline
LouW - great "speech" and a very good compilation of all what guys in aero labs are trying to tell us. Thanks.

(in reply to LouW)
       Post #: 80

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 6:48:21 PM   
Ben Lanterman



Posts: 1284
Joined: 10/27/2002
From: St. Charles, MO, USA
Status: offline
"As a wing moves at an angle through the air, the air above tries to move into the space vacated above the wing, however since it has mass, it doesn’t move instantaneously, but is accelerated toward the space. Two things happen. An area of reduced pressure is formed above the wing (Boyle’s law), and the affected mass of air acquires a downward motion. These things must happen together. The actions are inseparable. They are essential parts of the same action. One simply can’t exist without the other. One is not merely the by-product of the other but they are both necessary parts of the whole."

Lou are we talking about the same thing. I believe we have been using the terms like "deflected" to mean the downwash effects - as in the air above the wing is deflected into the low pressure area being developed. Yes the air flows over the wing, is accelerated, increases in velocity and the pressure above the wing is lowered. Then the air above is accelerated into the low pressure just as the wing is accelerated toward the low pressure. We aren't saying that one can't exist without the other. The fact is indeed that the downwash is a by-product of lift, it reaches it's maximum when the pressure field on the wing (and lift) is at a minimum. Because they both happen does not mean that the downwash is accelerating the CG of the wing. The fact is also that the air flowing around the leading edge of the wing, that is accelerated is at a maximum velocity when the low pressure is at a maximum.

Lou - what is accelerating the CG of the wing? It's F=ma. simple and direct. Where did the force come from? The sum of the forces on the wing must come from the OPPOSITE direction that the wing moves isn't it? The wing moves up or at least stays level with respect to 1g gravity acceleration. Which direction and what magnitude must the force on it come from? It is simple vector math. It must come from the bottom. There is no downwash on the bottom causing an up force is there? What is there to cause the up force - the answer is pressure.

You might think of it as details but I tend to think of it as the accurate statement of what is happening and everyone can understand it until someone comes by like Jeff and says something that is wrong, not a way of looking at it but in the most basic sense of everything you or I have studies, is wrong.

"The fact that engineers tend to deal with the part that is easier to measure and calculate, and ignore the rest, doesn’t make the rest any less true."

That is meaningless with respect to what we are discussing.

"Without the deflection (acceleration) of air there can be no pressure field developed therefore no lift. It’s really that simple."

If you are talking about the air going over the leading edge of the wing, following the countours of the wing, being accelerated and increasing in speed causing a low pressure area and calling that process "deflection" then it's true. I think from the first paragraph in this discussion we have all agreed with that.

Unfortunately some readers will think the deflection you are talking about is the downwash term. Look back at the drawing I made. What isn't clear about it? I have always differentiated the two processes at least by terminology. Don't confuse Leszek_K any more than necessary without defining your terms a little better.

< Message edited by Ben Lanterman -- 2/17/2005 7:21:34 PM >



_____________________________

Ben Lanterman

(in reply to LouW)
       Post #: 81

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 7:17:16 PM   
Ben Lanterman



Posts: 1284
Joined: 10/27/2002
From: St. Charles, MO, USA
Status: offline
A lot of back peddling going on. You said,,

"By the way - a rocket engine does not work on a pressure principle - it expells a mass of gas with certain velocity to create a reaction called (in this case) thrust. It just happens that in classic rocket engines a high pressure and a nozzle are required to make it efficient. Remember ion engines.
Again - remember ion engines. And no pressusre in a chamber - actually no chamber at all. "

But indeed the rocket does work on pressure. A solid rocket of the most simple kind has the nozzle and comuston chamber the same thing - a bottle rocket for example. When you mix the fuel and oxidizer in the Nozzle then the location is moved but the principle is the same.

Move the CG/mass of the rocked you must accelerate something and that requires a force. If the force is a million hot molecules bouncing on the nozzle shell we call it pressure.

Ion engines. Ever hear of the concept of the solar sail. It works on the principle of light pressure on a large surface. If I have an Ion rocket in outer space and I need to move the mass of the rocket, yes indeed Newton is there with F=ma. Moving the rocket mass is called acceleration. It takes what? Well a force. Take an ion with it's low mass, accelerate it through a magnetic field attached to the rocket and a small but useful force is applied to the rocket. Do it enough and you have the ion rocket. What do you call a bunch of mass particles (the ions) that have energy of motion - why we call it a pressure just like our air molecular setup at a given temperature. pv=nrt if I believe. It relates pressure, volume and temperature.

It is all pressures and forces making masses move with accelerations.

"Talking about a pressure in a combustion chamber being source of trust, I think Mr Pascal would disagree with you. "

I don't think Mr. Pascal would disagree with me, I put that in the comment to cover the case like the bottle rocket. Draw a combuston chamber that looks like a soda bottle. The hole in the outlet of the chamber allows the pressure of a given size area at the other end of the bottle to react the pressure in the chamber, so indeed it can work.

"Anyway, I think this discussion got quite hot, and not constructive at all. "

It is very constructive if it stops some of the mis-understandings of the basic laws that airplanes work under.

"Our planes will fly no matter who is guilty - Bernoulli or Newton.
Just moved to a new house so need to setup my workshop - and this is my priority now. "

Our planes will fly yes, but unless we make an effort to understand why we might as well swing a dead black cat around our heads before each flight and say that is what made the airplane fly. Ignorance done on purpose is never an excuse for bad understanding of our environment or the things happening in it.

< Message edited by Ben Lanterman -- 2/17/2005 7:22:14 PM >



_____________________________

Ben Lanterman

(in reply to leszek_k)
       Post #: 82

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 7:59:42 PM   
leszek_k


 

Posts: 30
Joined: 7/25/2003
From: Dubai, UNITED ARAB EMIRATES
Status: offline
Ben - I give up. Sombody has to stop that.

(in reply to Ben Lanterman)
       Post #: 83

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 8:43:17 PM   
bdavison


 

Posts: 3333
Joined: 8/23/2004
From: Warner Robins, GA, USA
Status: offline
"Ignorance done on purpose is never an excuse for bad understanding of our environment or the things happening in it. "

BRAVO


_____________________________

teamflyingcircus.com

(in reply to leszek_k)
       Post #: 84

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 8:50:18 PM   
Dave_Gherardini


 

Posts: 113
Joined: 1/25/2003
From: Central, IL, USA
Status: offline
Well, Im going to show some lack of knowledge in this area agin. But im curious about ground effect and when a wing gets in it what is actually going on. Is the downwash acutally what you feel or is it comming from the front of the wing. Im not sure if i termed that right but what i mean is, Is the air being squished closer to the front of the wing or is it the downwash being bounced of the runway. I have never felt this ground effect as far as i know but my brother who flys alot talks about it sometimes.. I hope this isnt to far off topic but ive always wondered what is acutally happening and why. Thanks again



Dave G
Home of the Carbon Cobra
http://www.dgmodels.rchomepage.com/dgmodels.htm

(in reply to leszek_k)
       Post #: 85

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 9:25:27 PM   
dick Hanson



Posts: 9920
Joined: 12/12/2001
From: slc, UT, USA
Status: offline
You don't need a degree to figure out the useful parts of all of this .
And it really can be fun to see what is happening.
Here is an example and I am certain one of the graduate aero engineers will provide the correct answer and in a simple form with no graph or math.
Visualize a glider making a flat gentle landing in dead calm air , on a dry , very dusty lakebed. (my story ,so it can be very dusty)

As the craft gets very close -- what happens to the dust?

Is there a forward movement of the dust?
Does dust behind the wing move first?
Or ---Is it simply unaffected?
Why?

< Message edited by dick Hanson -- 2/17/2005 9:28:43 PM >


_____________________________

I am watching you
Libby

(in reply to Dave_Gherardini)
       Post #: 86

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 9:39:40 PM   
bdavison


 

Posts: 3333
Joined: 8/23/2004
From: Warner Robins, GA, USA
Status: offline
If you want to feel ground effect, fly a heli...You'll know what it is like the first time you try to land. Its not technically ground effect, but it will give you an idea of what its like.. It can also on occasion be "felt" in model airplanes too. The result is normally an overshot landing in which the plane ends up "seeming to float" on a landing attempt while its about 6-7" off the deck. Many times pilots dismiss this as "I came in a little to hot".

My dad had a scratch built pattern plane a while back that was darn near impossible to land. Everytime he came in for a landing, that thing would float for miles on the ground effect "cushion" of air.

I wouldnt say ground effect is a result of the the leading edge, or downwash. I would say its more of the air being compressed between the wing and the ground. When the pressure increases, it pushes up on the bottom of the wing more. This pressure can actually get so high as to lift HEAVY objects off the ground. Race car drivers know about this.

_____________________________

teamflyingcircus.com

(in reply to Dave_Gherardini)
       Post #: 87

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 10:45:14 PM   
Ben Lanterman



Posts: 1284
Joined: 10/27/2002
From: St. Charles, MO, USA
Status: offline
Dave, ground effect when applied to a airplane landing or taking off is when the airplane, usually at a large angle of attack is close enough to the ground that the normal high pressures underneath are increased. Remember the air is limited on how fast it will move out from under the airplane and its wings by the speed of sound. So the pressures build up and the airplane "floats" on the "bubble" of high pressure. Dave if you were able to move under the wing at the speed of the airplane (just a little less so you would move aft) as the leading edge came close to you your ears would pop from the increased pressure. As it went over the pressure would stay high and then just as the trailing edge went over the downwash would really buffet you around and the ears might crack as the pressure is decreased again. Downwash shouldn't be underestimated, with luck it can knock over stuff.

Remember for a 10 ton airplane that is flying that the net result behind the airplane is 10 tons (plus or minus a couple of tons) of air being blown down (not sucked down by the wing but blown down by the pressure far above the wing). That is a proper wind most anywhere. No doubt somewhere there are sites where numbers are determined for the downwash of something like a jumbo jet.

Dick's comment about the race cars that had a fan built in to additionally "suck" (there is that term again!) or better to say to encourage the air to escape faster is to let the pressure vent and remove the lifting effects of the ground effect on the race cars.

OK dick I will guess although I have never actually been on a dry lake - but assume lots of dust - No doubt it gets blown all over the place aft of the wing because the downwash is strong to say the least. If you are going subsonic some high pressure will be propagated forward and depending on the relative forward speed the high pressure under the leading edge of the wing will probably nudge some dust up in front of the wing. I would guess it would look like it is spouting all around the wing edge but will have a lot of action aft of the wing as the downwash hits the ground. I have seen something like it with airplanes and snow on a runway. Watching cars on a highway in the rain is the same stuff going on. Of course there are the really big tip vortex actions as the high pressure underneath wraps around to the lower pressure on top and makes like a small tornado. That is going to whack the ground and make for neat dust blowing in the swriling pattern.

As a youth I built a radio controlled ground effect machine for my senior science fair project. It didn't crash as bad as a airplane did. It was a McCoy 29 racing redhead rear induction powered monster. It would lift and looked sleek but control was nonexistant with a single channel pulse system driving a very small rudder. The mechanics of the machine were way ahead of the control systems available to my improverished youth. That was in 1960.

Did I pass?


_____________________________

Ben Lanterman

(in reply to bdavison)
       Post #: 88

RE: Jef Raskin article on aerodynamics in Fly RC Magazine - 2/17/2005 11:49:35 PM