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trebuchet03 02-21-2008 06:16 PM

A Crash Course in Aerodynamics and an Introduction to Turbulence
 
Rather than sporadically give information in posts... Let me take a moment to explain a few things with respect to aerodynamics, cD and a few terms that go with that.... Basically, I'm about to regurgitate some of the concepts you might learn in a fluid mechanics course (but minimizing the math component)

First, some definitions,

Reynolds number: a ratio between the inertial forces (momentum of the working fluid) to viscous forces (property of resistance to shearing) | dependent on: body length, fluid velocity, fluid density, dynamic fluid viscosity, kinematic fluid viscosity. Reynolds number increases with length (all else equal) - once a certain region of Reynolds number is passed - you're in the turbulent regime. Do not pass go, do not collect $200 - it's over. This is why race cars generally don't have long boat tails. Instead, designers find where the transition zone occurs, and chops away. The extra weight and length (for maneuvering) isn't necessarily paid back from the aero benefit. <--- this does not apply to a streamliner made to only go straight.

Frictional Drag: this is the drag between the moving fluid and relativity stationary surface. May be referred to as viscous drag - I'll switch back of forth most likely. This value is dependent/sensitive on the Reynolds number.

Pressure Drag: this is the drag as a result of a pressure drop - wake. Think of that big blast of wind from a semi truck, or the waves generated by a boat. Pressure drag is mildly dependent on the Reynolds number, but generally not sensitive to it. Pressure drag is highly sensitive to body shape.

For both Frictional and Pressure drag.... It's important to note that they are both VERY dependent on fluid viscosity. That is, in inviscid (viscosity = 0) flow, both of drop to 0.

AoA: Angle of attack - draw a line in parallel to fluid flow. Now draw a line from the leading edge of a body to the trailing edge. Measure the angle between these two lines.

Streamlined Body: Drag losses are primarily due to viscous losses. Streamlined bodies of the same thickness are significantly more aerodynamic than a bluff body. Note that a streamlined shape doesn't necessarily mean a streamlined body - at a high AoA, flow separation causes great pressure drops.
Bluff Body: Drag losses at high Reynolds numbers are primarily due to momentum losses - meaning, pressure drop as a result of a wake.

Free Stream: This is the flow that is not impeded by a body.


Boundary Layer: I can spend a lot of time on this, but I'll abridge it... The boundary layer is the fluid directly beside the body. The general profile of the boundary looks something like this:
http://history.nasa.gov/SP-4103/p529.jpg
where the length of the lines represent a velocity vector - the longer the line, the faster the flow. At the point where the fluid meets the body, there is a zero slip condition. That is, at this point the fluid does not move. There are some important implications of this as it applies to differential calculus - but don't worry about that, just understand this concept ;) Below is the shape of the boundary layer (note that the y scale is increased for easier reading):
http://www.cartage.org.lb/en/themes/...s/img00032.gif
Note the several phases of the boundary layer:
  1. Laminar
  2. Transitional
  3. Turbulent
And just for fun - here's a real world example:
http://history.nasa.gov/SP-4103/p530.jpg

Laminar Flow: Fluid "layers" (streamlines) flow over each other in a parallel fashion smoothly over each other.
Transitional Flow: This is more of a mathematical zone as laminar turns into turbulent. I call it mathematical because there are specialized equations that apply to transitional flow only.
Turbulent Flow: The streamlines, instead of slipping over each other, diverge in chaotic eddies. Note that chaotic does not mean random, it "simply" means that it is highly dependent on initial flow conditions - small changes in these conditions create great differences in output.

Please note, there is no critical distinction between laminar, transitional and turbulent flow. The mathematical distinction is almost arbitrary - it's just a number that the community has agreed to use :thumbup:

Okay, I think that just about covers some minimal basics - if I make any knowledge assumptions, please let me know and I'll elaborate :thumbup: :thumbup:

I'm going to talk about bluff bodies for the most part as that's what our cars are (with exceptions - basjoos!).

So lets look at some simple objects and what happens.... A cylinder is a classic example:
http://www.flometrics.com/services/cylinder/cylslo.jpg
So, the flow in the front is generally nice, even and laminar. But downstream, there's some nasty eddies. The large vorticies off of a cylinder have their own natural frequency dependent on fluid velocity and cylinder diameter - coming at regular intervals. These remove energy from the body. The wake of a body typically has this same eddying motion, but not necessarily at a consistent frequency.

This is actually a VERY important phenomena as if this frequency matches the natural frequency of the cylinder (think a street lamp pole), the cylinder will vibrate divergently and without control it will eventually self destruct (Tacoma Narrows Bridge anyone?). This is why many light poles, especially in wind prone areas, are tapered. Additionally, power lines may have spoilers and damping mechanisms attached. Even large sky scrapers have vibration control for wind induced motion - one method uses VERY heavy weights (think tons) on the top floor of the building; given a certain wind speed, oil is pumped under the weights so they can move (constrained and attached to the structure by springs)...

How about a sphere?

http://www.princeton.edu/~asmits/Bic...R_combined.GIF

The sphere on the left (a) shows what happens with laminar flow. As soon as the pressure drop becomes significant you get separation, bugger.

So what's the deal with the picture on the right? How did we delay separation? That sphere has a trip wire. What does a trip wire do? It perturbs the boundary layer, a lot. Enough so that nearly the entire boundary layer in contact with the sphere is turbulent.

So how does this change cD? Here's some graphics:
http://www.princeton.edu/~asmits/Bic...oefficient.GIF
cD versus Reynolds #

http://www.princeton.edu/~asmits/Bic...w_patterns.GIF
Points on the graph above correspond to the letters below each case.

"Whoa Whoa Whoa!! Are you telling me cD changes with velocity?"
Yes, yes I am - but don't get too excited as this mainly applies to small objects. cD drops significantly as the Re# increases. BUT, it remains nearly constant for large Re#'s in the laminar region and approaches a constant value after the transitional region. As a car is very wide compared to something like a tennis ball, the Reynolds number is high - very high in fact (on order of 10^6 @ 55mph and 10^5 at ~3mph).


Balls!
Sports balls, believe it or not, have some great design... Smooth balls are not very efficient aerodynamically. This is why golf balls have dimples, tennis balls have fuzz, cricket balls have a stubby seam, baseballs have stitches, American footballs are textured, soccer balls have seams (Everywhere). Okay, some of this is traditional - but it still plays a role.
http://www.princeton.edu/~asmits/Bic.../roughness.GIF
Roughness and cD... Having a bit of roughness induces turbulence. Look at the photo above of the sphere with the trip wire - surface roughness is very similar, in effect, to a trip wire.

This results in a reduction of cD as shown in the above graph (which just so happens to also be in my fluid mechanics book - Fundamentals of Fluid Mechanics produced by John Wiley & Sons :p). Relative roughness is t/D, t being the thickness of "rough" and D being the diameter of a sphere/cylinder. The dashed line on the left is a golf ball.

And on the subject of golf balls... why? The dimples! Why? The dimples act, in effect, like a trip wire. They promote a transition to turbulent flow. By doing so, we get higher skin friction (yet another name for viscous losses). BUT, remember the definition of a bluff body? A golf ball is a sphere - and spheres are bluff bodies. Most of their losses come from the wake - so if we can move the wake further back, we can reduce the wake size and reduce the losses from the wake. It just so happens that by increasing the turbulence, you decrease your drag by reducing where most of the drag is coming from - flow separation (wake).

------
Okay, so what's all of this talk about the benefits of turbulent flow? Turbulence is the most misunderstood concept with regards to aerodynamics, in my opinion. Nature has known for millions of years of the benefits of turbulence. This is why dermal denticles on sharks help lower their cD. Likewise the bumpy tubercles of a whale fin. etc.
http://www.whalepower.com/drupal/fil...mpback_fin.jpg

The key difference between induced turbulence and the turbulence as a result of a shape is the size. Larger eddies, swirls, etc. contain more energy than smaller ones. So if we induce smaller eddies, with a small amount of energy - we move into the turbulent regime without a whole lot of loss that you'd typically associate with the word "turbulence". This will typically be referred to as "energizing the boundary layer." This can happen on a very VERY small scale - the smallest of which is the Kolmogorov micro scale. <-- keep in mind that the mathematic description of turbulence is not solved - we just can't do it, yet :p

Some very notable physicist when asked what they would like to ask God have replied:
Werner Heisenberg: "When I meet God, I am going to ask him two questions: Why relativity? And why turbulence? I really believe he will have an answer for the first."
Horace Lamb: "I am an old man now, and when I die and go to heaven there are two matters on which I hope for enlightenment. One is quantum electrodynamics, and the other is the turbulent motion of fluids. And about the former I am rather optimistic."
^^both of these were mentioned in my lectures :p

--------
Vortex Generators.....
Okay, so I've been building up to this as it has come up a lot recently - trying to give some background before I get to it.

Here's the answer to some straightforward (I hope) questions:
1. Does it increase turbulence?
Yes - the idea is, move the wake back with turbulent flow
2. Does it reduce cD?
The devil's in the details. Properly applied, absolutely yes. Nature has proven this through millions of years of evolutionary change. CFD and tunnel testing too :p Keep in mind, a vortex generator is a band aid on an object with poor aerodynamics. Vortex generators are not solutions, just "well, we screwed up - lets throw this on." You the designer need to practice intelligent design. I don't mean the type where only one dude made everything or whatever you want to believe - I mean thinking through, validating and backing up claims and research as to why your design is superior ;)
3. wtf counts as a vortex generator?
Almost anything that perturbs flow - from commercially sold tabs to dimples to stiff fuzz (think tennis ball). Vortex Generator does not necessarily refer to one particular product (nor do I endorse any such product).
4. How much improvement?
See #2 - Mitsubishi has published a paper reporting a cD reduction of 6 points (.006) on a Lancer which can be considered significant in the cD world. They used delta wing type vortex generators placed 100mm in front of the predicted separation point:
http://www.primitiveengineering.com/..._effect_vg.jpg
http://www.primitiveengineering.com/...vortex_top.jpg

Note the smaller wake size and how the separation point is further down the rear glass:
http://www.primitiveengineering.com/...ex_gen_cfd.jpg

---------
Wunibald Kamm
Here's a gallery of creations by Wunibald Kamm. Think of it as functional aerodynamics. Notice the VERY smooth transitions from hood to windshield (in most cases). Also note the placement of engine bay discharge - either directly in front of the windshield or through submerged ducts on the side.
Site (in German but with lots of aero porn)


Some Links for you....
Basjoos' Car - What we should be doing...
tasdrouille's Link Dump
Side Mirror Drag Quantized - .030
Aero Truck Bed Cap



Whew, freaking long.... Questions/additions? Let me know if I missed a typo too :)


Next mega write-up... The physics of friction - to dissuade some myths about rolling friction versus static friction etc.

MetroMPG 02-21-2008 06:43 PM

AWESOME writeup. Thanks for posting that.

---

Here's a question: Is there a simple answer as to why introducing a small amount of turbulence in the boundary layer (ahead of the area where flow would normally separate) moves the separation point further downstream & reduces the size of the wake?

Or does that fall into the category of thinking up questions to ask god? :P

bestmapman 02-21-2008 07:12 PM

Nice article. Good graphics.

Fuzzy 02-21-2008 08:06 PM

Quote:

Originally Posted by MetroMPG (Post 10862)
Here's a question: Is there a simple answer as to why introducing a small amount of turbulence in the boundary layer (ahead of the area where flow would normally separate) moves the separation point further downstream & reduces the size of the wake?

Treb can correctly me if my rusty aero is wrong; but it has to do with "re-energizing the boundary layer." It's separating because the friction is removing energy from the flow. The turbulence draws in flow from outside the boundary layer which has higher velocity, which will keep it attached longer. A simpler explanation could be "mixing."

Big Dave 02-21-2008 08:34 PM

Good job of chopping through a number of sources and putting it in a nutshell.

Something else. If you think of it, the vehicles of the folks on this site operate in a fairly small air speed range and are all (very) roughly the same length, so the Reynolds numbers will be fairly close. Compared to the Reynolds number range for aircraft the envelope we are talking is tiny.

trebuchet03 02-21-2008 09:16 PM

Quote:

Originally Posted by MetroMPG (Post 10862)
AWESOME writeup. Thanks for posting that.

---

Here's a question: Is there a simple answer as to why introducing a small amount of turbulence in the boundary layer (ahead of the area where flow would normally separate) moves the separation point further downstream & reduces the size of the wake?

Or does that fall into the category of thinking up questions to ask god? :P

Fuzzy is pretty close... So yes, it's called "energizing the boundary layer." Viscous friction slowly increases the thickness of the boundary layer. When this happens, think of an ocean wave crashing over itself and in the case of air, it's making an eddy.

So the simple answer is - you're taking some fast moving energetic air and sweeping it into the slow boundary layer to give it a little kick.

Keep in mind that the type of turbulence we're introducing isn't like the rolling eddies off of a car (or semi truck), it's tiny little ones :thumbup:

Fuzzy 02-21-2008 10:52 PM

Quote:

Originally Posted by trebuchet03 (Post 10858)
(but minimizing the math component)

No pun intended? ;)

I missed this and the 'energizing flow' bit 'cause I skimmed this while I was still at work.

brucepick 02-21-2008 11:59 PM

:thumbup: :thumbup: Make this article a sticky.

mattW 02-22-2008 02:36 AM

That's such a useful post. Do you mind if I 'borrow' some of your content for my EV wiki? I've got a whole section devoted to Aerodynamics including theory, projects, testing and articles but its pretty basic at the moment. There's a small topic on rolling resistance too if you want a starting point.

Daox 02-22-2008 10:43 AM

Great post. I especially like the explination of VGs and why they work. :thumbup:

Gone4 02-22-2008 01:19 PM

If you want a good explanation of secondary flow there is a cool video on youtube. It cuts off the more interesting parts that occur later, that you can find on MIT's OCW

http://youtube.com/watch?v=HKG9aPRldPs


It's possible to used vanned diffusers to reorganize the flow without introducing turbulence, which the video delves into later if you go beyond the clip on youtube. For cars the vortex generators are about closing the flow on the pressure differential down, not actually assisting the flow. That is the turbulent flow interrupts the pressure differences caused by the sudden termination of the body. This is done by adding a swirl component; this is abstracted by the Euler-N equation and others. The swirl causes a theta differential in the flow direction that disrupts laminar flow that causes the wake.

My graduate studies are focused on fluids, and more specifically turbomachinery right now. I fully intend to concentrate on heat transfer in the future, so this isn't quite my first love but I should be able to help.

trebuchet03 02-22-2008 01:45 PM

Quote:

Originally Posted by Daox (Post 10958)
Great post. I especially like the explination of VGs and why they work. :thumbup:

Careful - just slapping them isn't any qualification for if they work... Or just looking at the car and placing them isn't really a qualifying factor either unless you put them on, test, adjust, test etc. No doubt, Mitsubishi went through several iterations to find their location...

Quote:

Originally Posted by Fuzzy
No pun intended?

100 imaginary cookies for you :D

KWillets 02-22-2008 02:56 PM

Aerodynamics is fun. I once had a job doing wind tunnel tests, and it's a tricky business. One thing I learned is that most of the terms like Cd are approximations made up to fool amateurs. Classical fluid dynamics is all steady-state stuff where a body is assumed to reach an equilibrium state with a steady flow around it. "Turbulence" (another loosely defined term) is treated as an untidy exception to that.

One note about your example: that's a supersonic test. The lines are shock waves; the angle suggests it's moving at about Mach 2. You might want to find a subsonic example.

Reynolds number is difficult to explain, but it's basically a scaling factor between the body and the intramolecular distance of the gas. At small scales, turbulence is disproportionately less likely to occur, while large bodies have many more eddies to deal with.

Most of aerodynamics is about flow visualization. There are many tricks to getting smoke trails, pressure sensors, etc., around the model to get useful measurements. The good news is that empirical tests work -- theory is sort of a starter course on where problems occur, but the state of the art is a lot of testing and fiddling.

trebuchet03 02-23-2008 03:02 AM

Quote:

Originally Posted by KWillets (Post 10991)
One note about your example: that's a supersonic test. The lines are shock waves; the angle suggests it's moving at about Mach 2. You might want to find a subsonic example.

Yeah... I was hoping no one would notice that :D If I find a better picture, I'll replace it (I'm looking for something that points to each regime like that one :p).

aerohead 02-23-2008 03:37 PM

turbulent boundary layer
 
Quote:

Originally Posted by MetroMPG (Post 10862)
AWESOME writeup. Thanks for posting that.

---

Here's a question: Is there a simple answer as to why introducing a small amount of turbulence in the boundary layer (ahead of the area where flow would normally separate) moves the separation point further downstream & reduces the size of the wake?

Or does that fall into the category of thinking up questions to ask god? :P

The question is a good one and before I try to answer,I'll go home and look it up.It has to do with ideal fluids,invisid flow Daniel Bernoulli's velocity/pressure relationships,momentum interchange,friction,pressure,density,etc..The reason I haven't committed
it to memory,is that from my understanding,our cars live in a world of turbulent boundary layer for their size and velocities whether we like it or not,and there's nothing we can do about it.

Above 20-mph we have the dimpled golfball scenario working for us,and drag coefficients are stable up to transonic flow(about 250-mph).

Submerged in the troposhere,as our cars move and displace larger and larger volumes of atmosphere,air at rest is accelerated until it reaches the point of frontal area for each vehicle.Remember,up to this point,it is in a positive pressure gradient,ramming the air.As the air reaches the frontal area,or area of greatest cross-section,it no longer resides in a region of positive pressure.If air was an ideal fluid,it would have no friction,and its velocity-pressure(Bernouli) would simply be converted back to static-pressure(Bernoulli).

Because of energy loss and heating due to viscous shearing within the laminations of air close to the skin of the car,thermodynamics dictates that entropy will scuttle our attempts to get the air back as it was before we came along.Subsequently,the flow will "stall" and separate from the car,creating a turbulent wake of high drag.

Slick as it is,the smooth polished paint of our cars has enough surface roughness to "trip" the air into tiny burbles,which as members have noted,feed kinetic energy into the layer of air adjacent to the skin of the car which is otherwise at a standstill,and will postpone the point of separation,say for the golfball,well behind the point of maximum diameter,thereby reducing its wake,cutting drag by half,and extending range from 150-yards,to 300-yards with a clubhead exit velocity of 110-mph.

If someone doesn't beat me to it,I'll dig out the details for next time.Main point is, that we couldn't have a laminar boundary layer if we tried.


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