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  1. #1
    Veteran Member Four Rings DRAKLORE's Avatar
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    Post CFM vs. PSI an informative thread**

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    So here's the topic, I noticed a lot of members cannot differentiate between PSI and TURBO efficiency, because I see a lot of you thinking it's the PSI that makes the power. For those members I'm about to BLOW YOUR MIND!!!

    For some it may seem common knowledge that a small turbo let's sat a KO3 at 20psi, will not produce the same power as a larger turbo (say a GT3071) @ the same 20psi.
    This is because the larger turbo has a higher CFM at the same psi.
    CFM= cubic/feet per minute and is a MEASURE OF VOLUMETRIC FLOW (sorry for the confusion)
    PSI= pound/square inch and is a measurement of Pressure

    Because the larger turbo has a larger turbine it
    1.has a higher rotational mass, therefore takes longer to spool up.. Hence LAG
    2.Has bigger "blades" on it's compressor wheel, therefore it does not need to spin as fast to produce the same CFM as the smaller turbo

    Because smaller turbos spin faster they in turn heat up the air quite a bit more, thus the need for a more efficient I/C setup
    Larger Turbos use larger wastegates with larger springs. The wastegate is essentially an alternative route that exhaust gasses can take to exit the manifold. turbo uses the spent exhaust gasses as the flow out of the engine to spin a compressor wheel (common knowledge correct?) but some do not know that the wastegate is there so that when the turbo is not needed to create boost, it can reroute or partially reroute the exhaust gas around the turbo in effect causing less/lower CFM.

    Here is an excerpt from CHAD on starquestclub.com (regarding CFM vs.psi)
    It's very dynamic, the whole thing is driven by exhaust volume and pressure on the turbine wheel, which is dictated by the CFM's the motor is drawing in, which is forced in by the comperssor wheel. You can't have one without the other, and they both effect each other.

    It's nearly impossible to predict any specific scenerio of x + y / z * w = a where you have pressure, CFM, RPM's, effeiency, and resulting power.

    It's more of a relationship thing than an exact science.

    yes, a small motor with a lot of exhaust pressure will cause a turbo to build boost due to bottle necking, but then a small motor won't likely be able to make enough exhaust pressure to accomplish this task in the first place.

    What you are describing there is a function ot turbine wheel to compressor wheel size ratios. If they are perfectly suited to the task they can do just about anything , but it's all tradeoffs.

    If you take 2 turbos where one is exaclty twice the flow as the other, the smaller one will make boost sooner and easeir, and the larger will be later but improve topend power. If you compare HP at a the same pressure, the larger one will higher overal, but the smalelr one will accomplish it peak lower in the RPM band. The large one represents less resistance to exhasut flow, and is thus going to make more power for a given PSI. that is why bigger turbos spool later, but make more power. Because they make more power and flow more, they also have more exhaust pressure/volume, which adds even more to the equasion and shows up as increased power output for a given (equal) pressure.

    It's like a 3 dimensional relationship.
    CHAD again..
    Yah, I'd actually argue 5 dimensions since temperature is also a large factor. It's just hard to visualize 5 dimensions

    The point is that it's not a linear relationship, and there are more than 2 variables in the origional question.

    It could be argued there are dozens of varriables, such as A/R of of the housings and wheel trims, geometry of the manifold, speed and temperature of the exhaust, B.S.F.C. of the engine, elevation, etc.

    Shaft speed is also important, air can only move so fast, a bigger turbo can move a given volume of air with a lower shaft speed, so they are far more efficent at high levels compared to a smaller turbo asked to do the same task. That is in part where a lot of the heat problems come from on small turbos turend all the way up, where a bigger turbo is probably a better choice.

    Compressor maps are used to determine the CFM/PSI efficiency of turbos at given RPMS (of turbo)
    And can be very useful when determining what turbo would be most effective for your project car.
    Example:


    WIKIPEDIA "compressor map"

    Now I know this has been discussed in other sections and forums, but I thought I'd give the B7 crowd a taste and hopefully I can get Sprode to introduce himself then maybe we can get this thing stickied***

    I will be editing this and adding so feel free to PM or post any misinformation or additional info you'd like to see.

    SHANE
    Last edited by DRAKLORE; 10-10-2011 at 05:39 PM.
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  2. #2
    Veteran Member Four Rings DRAKLORE's Avatar
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    Turbo basics-

    turbocharged system-



    What's a "compressor wheel"? You may ask. Well think of a window fan, when the fan is off on a windy day the air rushing in past the fan blades make the fan spin. This is essentially how your turbo works, doing so with exhaust gasses <outside wind flowing past a turbine or "compressor wheel" <window fan

    Bigger turbos have bigger wheels, bigger wheels in turn require a bigger housing. Here's a little comparo



    So now that your starting to understand a few aspects let's start looking at some compressor maps.(lol)
    Carefully study each map,
    SEE how each turbo flows (CFM) more lbs/min at its peak efficiency the larger it is?!
    KO3 at peak efficiency flows about 10lbs/min!
    Then the KO4 at around 20lbs/min
    The GT2860 at roughly 25lbs/min
    And the GT3071 at approx 30lbs/min



    ^^^^^KO3^^^^^^^

    ^^^^^^^^KO4^^^^^^^

    ^^^^^^GT2860^^^^^

    ^^^^^^^GT3071r^^^^^^^



    I'll explain this in further detail later when im not as tired, that way it's a little less of a jumbled mess of info and a little more precise. Sorry If any info is a misrepresentation as it's 1:30AM


    SHANE
    Last edited by DRAKLORE; 10-10-2011 at 08:11 AM.
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  3. #3
    Veteran Member Four Rings DRAKLORE's Avatar
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    Air density/elevation

    I'm going to leave the other topics open for discussion and will modify them at a later date.


    Here is some info pulled from
    Boosting Your Knowledge of Turbocharging
    By Randy Knuteson
    A i r c r a f t M a i n t e n a n c e T e c h n o l o g y - O C T O B E R 1 9 9 9

    Regarding air density and elevation, mind you the information was adapted for airplane turbocharging so some things IE:carburetors do not transfer lol
    FULL ARTICLE HERE


    Increased efficiency in a rarified atmosphere

    At sea level, the atmosphere in which we
    live and breathe is continually under a pres-
    sure of about 29.92 inches of mercury (Hg).
    At 1,000 feet, this “free air” drops in pressure
    to about 28.86 inches Hg. Air becomes pro-
    gressively less dense at all altitudes above
    sea level. Because of this, all naturally aspi-
    rated engines experience a reduction of full-
    throttle, sea level power output as they
    increasingly gain altitude. On a “standard
    day,” atmospheric pressure at 10,000 feet
    hovers at only 20.5inches Hg. In these con-
    ditions, a naturally aspirated engine is
    unable to sustain full power performance
    due to the lack of air density at these higher
    altitudes. Without the aid of a turbocharger,
    a loss of 3 to 4 percent of power or approx-
    imately 1 inch of MAP per 1,000 foot gain in
    altitude seems to be the rule.

    With the fuel to air ratio remaining con-
    stant, the amount of power developed by an
    engine is directly proportionate to the mass of
    air being pumped into the engine. On a non-
    turbocharged engine, an increase in airflow is
    achieved by changing the throttle angle to
    increase MAP, or prop-pitch to increase RPM.
    The atmospheric limitations of density alti-
    tudes coupled with the mechanical limitations
    of the engine and propeller pose as restric-
    tions to engine speeds. Some means of force-
    feeding the engine additional air is required to
    overcome these limitations........

    Pressures to Perform

    As their names suggest, Valves and
    Controllers both regulate and control tur-
    bocharger discharge pressure. This is an
    exacting science due to the fact that there is
    a disproportionate air/fuel ratio that must be
    tailored to the ever-changing demands of the
    engine as well as atmospheric density
    changes. For these reasons, a means of man-
    aging this forced air-flow to the cylinders is
    necessary to prevent the onset of detonation
    or overboost. The control portion of the tur-
    bocharging “system” was designed for this
    purpose. Valves and controllers provide the
    desired flight envelop, while keeping engine
    intake manifold temperatures and exhaust
    manifold pressures as low as possible.

    Deck Pressure and Manifold Pressure
    A basic knowledge of the air pressures asso-
    ciated with turbocharging is necessary for a
    more thorough understanding of these control
    systems. Air upstream of the throttle plate is
    often referred to as “Upper Deck Pressure.”
    Deck pressure is measured between the com-
    pressor discharge and the inlet to the fuel injec-
    tor or carburetor. Pressure downstream of the
    throttle is referred to as “Manifold Pressure” and
    is referenced between the throttle plate and the
    cylinder intake. A pressure drop occurs across
    the throttle plate and is dependent upon the
    position of the throttle angle. Deck pressure al-
    ways exceeds manifold pressure. At wide-open
    throttle, the air pressure drop across the throttle
    plate is at its minimum (as little as 1/
    4 in. HgA).
    And conversely, as the throttle is closed, this
    pressure drop increases. These pressures
    change both in response to throttle movements
    and variations in air density and temperatures.
    Air density is a function of both pressure
    and temperature
    . Therefore, air temperatures
    influence the upper deck and manifold pres-
    sures. As you recall, as air is compressed, it
    increases in temperature, resulting in a reduc-
    tion of air density and consequently a loss of
    engine power. A natural reduction of air densi-
    ty also occurs at higher altitudes and at tem-
    peratures above standard, which further exac-
    erbates this problem. The compressor is forced
    to work harder to feed a sufficient amount of
    air to the cylinders. Excessive heat becomes the
    undesirable by-product of this exchange.
    Generally, there is a loss of one percent of
    horsepower for every 6 to 10 degrees increase
    in induction air temperature.
    Remember,
    engine power is influenced not only by rpm
    and manifold pressure, but also by induction
    air temperature. In certain installations an inter-
    cooler acts as a heat exchanger to cool down
    this discharge air and recapture lost power.
    Last edited by DRAKLORE; 10-10-2011 at 08:17 PM.
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  4. #4
    Established Member Two Rings
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    Good Stuff, I'm having flashbacks from school. We used to have to figure out the forces on a compressor blade in a certain stage of a 6 stage turbine given the inlet and exhaust air temperatures, and the dimensions of the blade, BY HAND.. no calculators.. goddamn I don't miss that shit at all..



    Good Read Shane!

  5. #5
    Veteran Member Four Rings Solarsuplex's Avatar
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    Should use that reserved spot and ad a tl;dr. haha

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    Veteran Member Four Rings thenofjboy's Avatar
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    Good Stuff Shane! People will def benefit from this -
    Sean

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    Veteran Member Four Rings DRAKLORE's Avatar
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    Haha I guess not everyone is interested enough in it to read, but it's something that I like to try to be knowledgeable in!
    -Shane Drake-
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  8. #8
    Veteran Member Four Rings Sprode's Avatar
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    I have way too much to say on this topic to keep it coherent. You think his post was tl;dr...

    I'll put it out there that CFM doesn't necessarily mean velocity. Is really more like a measure of power potential. Saying CFM is a measure of velocity is really quite close to saying PSI is a measure of power because they both depend on geometry.

    This is a specifically important distinction when you talk about VTG turbos (or poor man's VTG like my supra has).

  9. #9
    Veteran Member Four Rings DRAKLORE's Avatar
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    Alright thank you Sprode!! Idk what I was thinking trying to make that sound coherent at 1:30AM lol
    Trying to sort it out, I left out the one topic I was trying to cover which was air density....
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  10. #10
    Veteran Member Three Rings Homer's Avatar
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    Quote Originally Posted by Sprode View Post
    I have way too much to say on this topic to keep it coherent. You think his post was tl;dr...

    I'll put it out there that CFM doesn't necessarily mean velocity. Is really more like a measure of power potential. Saying CFM is a measure of velocity is really quite close to saying PSI is a measure of power because they both depend on geometry.

    This is a specifically important distinction when you talk about VTG turbos (or poor man's VTG like my supra has).
    A little thing that bugs me.
    CFM is a unit of flow rate of a given volume (volumetric flow). Cubic Feet per Minute.
    -Jacob
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  11. #11
    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by DRAKLORE View Post
    Alright thank you Sprode!! Idk what I was thinking trying to make that sound coherent at 1:30AM lol
    Trying to sort it out, I left out the one topic I was trying to cover which was air density....
    You will find that the density remains pretty much constant until air starts moving realllly fast

  12. #12
    Veteran Member Four Rings jimrobbington's Avatar
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    I have also noticed over time, that just because you have reached your peak boost through a specific gear, does not mean you have acheived maximum acceleration. The turbo can be at maximum performance, while at the same time the engine isn't. I think Chad was trying to touch on this maybe.

    Peak boost does not equal peak engine performance given a specific RPM, or situation.
    2021 Audi S4, P34 Intake

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    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by jimrobbington View Post
    I have also noticed over time, that just because you have reached your peak boost through a specific gear, does not mean you have acheived maximum acceleration. The turbo can be at maximum performance, while at the same time the engine isn't. I think Chad was trying to touch on this maybe.

    Peak boost does not equal peak engine performance given a specific RPM, or situation.
    "Peak boost" is limited by the wastegate. so, this is a true statement for the most part. But if you were driving a car good for, say 35psi, but can't even make that in first, it usually tracks pretty well. Once the wastegate opens, its all about your cams for peak performance. Really, its all about the cams anyway.

  14. #14
    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by Homer View Post
    A little thing that bugs me.
    CFM is a unit of flow rate of a given volume (volumetric flow). Cubic Feet per Minute.
    Yeah, he said that in the OP, but started talking about velocity. I forgot to show my work in explaining power potential. but I just woke up.

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    Veteran Member Four Rings Mc Suly's Avatar
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    Nice write up
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    Veteran Member Four Rings jimrobbington's Avatar
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    Speaking of air density, I completely understand the massive amount of power lost in NA engines at altitude, but how much power would I gain going down to sea level? Would it be noticable?
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    Veteran Member Four Rings CorneliusRox's Avatar
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    I'll be reading this later today :-)

  18. #18
    Veteran Member Four Rings DRAKLORE's Avatar
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    Quote Originally Posted by Sprode View Post
    You will find that the density remains pretty much constant until air starts moving realllly fast
    Sprode isn't cold air dense when compared to hot air? That is where I was going with that regarding larger turbos.....

    Please PM me with any info you want to add. That way we can put it in the reserved space, and keep it at the top. (I'll give you all due credit :-)

    Ps-I am learning here as well, I'm going to be editing the section about CFM and creating a better flow of information as we go.

    Shane Drake
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  19. #19
    Veteran Member Four Rings Sprode's Avatar
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    Unfortunately, some good questions do not have easy answer. The math involved in some of this even makes me blanch so I apologize in advance. You are noticing some differences between open and closed systems. Our intakes are considered closed for analysis.

    http://en.wikipedia.org/wiki/Compressible_flow

    http://en.wikipedia.org/wiki/Incompressible_flow

    Suffice it to say that outside of valve design, our engines follow an incompressible flow regime. Air would have to be moving ~500 ft/s give or take for the density to start changing in the flow calculation. Short of a lot more explanation than I can give right now, just assume that the density is whatever atmo is. The compression generates temperature increase proportional to delta T=delta Pressure/(Ideal gas constant*density). Obviously this is oversimplification, but will get within a few percent.

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    Veteran Member Four Rings CorneliusRox's Avatar
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    Sprode, I know you know more on this stuff than me, but it sounds like you are categorizing air as a non-compressible fluid.
    Where all non-compressible fluids are actually compressible after they reach the speed of sound (which is based on elevation largely).
    The density of air can be changed at any speed like when you squeeze an empty bottle, or when you reach higher pressure in your intake, unlike water which only has these behaviors at supersonic speeds.

    isnt this the case?

  21. #21
    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by CorneliusRox View Post
    Sprode, I know you know more on this stuff than me, but it sounds like you are categorizing air as a non-compressible fluid.
    Where all non-compressible fluids are actually compressible after they reach the speed of sound (which is based on elevation largely).
    The density of air can be changed at any speed like when you squeeze an empty bottle, or when you reach higher pressure in your intake, unlike water which only has these behaviors at supersonic speeds.

    isnt this the case?
    Intake airflow is nowhere close to sonic. What you are doing when you squeeze a bottle is creating a pressure difference, not a density difference. You said it yourself for the intake.

    If you read through those articles, incompressible flow assumptions work just great until high speed. I don't know much about supersonic hydrodynamic flow, but water is assumed incompressible for my underwater acoustics books too.

    A lot of what you are unclear on is addressed in the compressible flow link.

    EDIT: Maybe I'm not being clear. The density will rise, but we are talking about very small increases until well past bulk flow speeds that we see.
    Last edited by Sprode; 10-10-2011 at 12:25 PM.

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    Veteran Member Three Rings Homer's Avatar
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    Quote Originally Posted by Sprode View Post
    Yeah, he said that in the OP, but started talking about velocity. I forgot to show my work in explaining power potential. but I just woke up.
    It was this that caused me to stop reading in the OP's post.
    CFM= cubic/feet per minute and is a measurement of velocity
    I'm just glad there are at least a couple level heads in this forum.
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    Veteran Member Four Rings rongeur's Avatar
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    =CFM= cubic/feet per minute and is a measurement of velocity
    I have to agree with sprode in that CFM is related to velocity GEOMETRICALLY, but is not velocity in itself as it seems to be claimed by the OP. For example, if you hold the CFM constant and constrict the volume of the conduit it flows through (water, air or whatever), you will increase the resistance to flow and thus increase the velocity of the flow. Now if you do the opposite and increase the volume of the conduit and hold the flow rate constant, you will decrease the resistance to flow and also decrease the velocity. I think the point is that CFM is a measurement of volume delivered over time and velocity is a measurement distance over time.
    Last edited by rongeur; 10-10-2011 at 01:32 PM.
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    Veteran Member Four Rings CorneliusRox's Avatar
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    lol I didnt notice it was cubic/feet. Relax though, we all know what he meant.

    Sprode, I had a bad analogy. If you have a syringe with the end plugged and air on the inside and pushed on it, you would be compressing it, throwing more atoms closer, making more pressure, but also higher density. After all, elevation affects density only because of the weight of the air sitting on top of it's self (obviously because of gravity) which is the same concept as physically squeezing it.

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    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by CorneliusRox View Post
    lol I didnt notice it was cubic/feet. Relax though, we all know what he meant.

    Sprode, I had a bad analogy. If you have a syringe with the end plugged and air on the inside and pushed on it, you would be compressing it, throwing more atoms closer, making more pressure, but also higher density. After all, elevation affects density only because of the weight of the air sitting on top of it's self (obviously because of gravity) which is the same concept as physically squeezing it.
    You are correct in the case of a closed system. Ideal gas law, in most useful form to me is P/rho=RT. The percentage change of pressure and density would be the same in a closed syringe. Temperature would not increase much as long as you changed the volume slowly. A temperature loss would manifest itself as a ever lowering pressure. Without mass flow, the density would be completely constrained by the volume.

    There are a lot of concepts being thrown around out here. It is also getting to the point where it would require me to start drawing diagrams. Luckily enough, NASA has done some of this for me. Boyles law (half of ideal gas law) states how a confined gas reacts to a change in volume. This assumes no heat transfer to the environment. Keeping Temperature constant makes it a reversible process, and allows the use of Ideal Gas Laws.

    http://www.grc.nasa.gov/WWW/k-12/airplane/boyle.html

    Open systems with internal flows follow very different and far more complicated models.

    There is enough here to keep all of you busy for a long time. I will try to answer questions.

    http://www.grc.nasa.gov/WWW/k-12/airplane/shortc.html

    Beats the hell out of wikipedia. http://www.grc.nasa.gov/WWW/k-12/airplane/machrole.html This one goes into detail about why I considered air incompressible. EDIT: also this http://www.grc.nasa.gov/WWW/k-12/airplane/isentrop.html
    Last edited by Sprode; 10-10-2011 at 04:45 PM.

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    Site Moderator Four Rings kristokes's Avatar
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    Great thread, Shane

    I will move this into the B7 A4 Tech sub-forum in a few days.
    Stokes - Site Moderator, Audizine

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    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by kristokes View Post
    Great thread, Shane

    I will move this into the B7 A4 Tech sub-forum in a few days.
    Where it will die a slow death. Leave it here till it actually dies IMO.

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    Site Moderator Four Rings kristokes's Avatar
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    Quote Originally Posted by Sprode View Post
    Where it will die a slow death. Leave it here till it actually dies IMO.
    Because not everyone has access to the B7 A4 Tech sub-forum.
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    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by kristokes View Post
    Because not everyone has access to the B7 A4 Tech sub-forum.
    Mod's know best. But I click on the tech forum once every 10 days or so, and it has 3 posts this month....

    EDIT: oops, 4 posts.

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    Veteran Member Four Rings Sprode's Avatar
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    Quote Originally Posted by jimrobbington View Post
    Speaking of air density, I completely understand the massive amount of power lost in NA engines at altitude, but how much power would I gain going down to sea level? Would it be noticable?
    I'm surprised I missed this one. The altitude doesn't hurt you because it helps the turbine (in theory) just as much as it hurts the compressor (normalizing efficiency). I'd love to see some back to back dynos but I haven't seen much. NA cars have no turbine, so they just get hurt. Reduction in exhaust backpressure does not nearly make up for it.

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    Veteran Member Four Rings DRAKLORE's Avatar
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    Sprode- let's break this down into lamens terms. I know not an easy task but your even losing me and I'm trying incredibly hard to understand lol

    So we know atmosphere at higher elevations is "thinner" which equals a loss in power due to the fact that more oxygen molecules create more power <simply speaking!?

    Turbo cars do not suffer as much of a loss because they in a sense create their own atmosphere?

    There is a difference between compressible flow and non compressible flow. Water is generally considered non compressible.
    Because the air flowing through intake has a place to go (essentially) it is considered a flow and this non compressible?

    Because the turbo only creates positive atmosphere when it's flowing a higher CFM than the intake system can handle. Essentially putting the air in faster than the engine can expell it?

    Is this the reasoning behind making the exhaust ports smooth and intake ports rough?
    Amongst other things I'm interested in how different bottlenecks in the intake system affect the air density ad it flows into the chamber. Like going from a 2.5"I/C piping to Some sloped endtanks with a large pressure drop then back to 2.5" piping...

    In my offhand experience, A/C systems use a similar pressure drop scenario to drop the temperature of the flow.
    If some of the physics transfer over would it make sense for me to have 2.5" IC piping to FMIC then 3" piping to a 3" TB and intake? Or will 99.9% of the cooling be from the FMIC as I suspect?
    Additionally it seems other people from my researching are bigger supporters of the larger turbo denser cooler air theory...

    Please let's not let this thread die just yet in the tech section. Personally never even been there lol

    Shane Drake
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    Quote Originally Posted by DRAKLORE View Post
    Sprode- let's break this down into lamens terms. I know not an easy task but your even losing me and I'm trying incredibly hard to understand lol

    So we know atmosphere at higher elevations is "thinner" which equals a loss in power due to the fact that more oxygen molecules create more power <simply speaking!?

    Turbo cars do not suffer as much of a loss because they in a sense create their own atmosphere?

    There is a difference between compressible flow and non compressible flow. Water is generally considered non compressible.
    Because the air flowing through intake has a place to go (essentially) it is considered a flow and this non compressible?

    Because the turbo only creates positive atmosphere when it's flowing a higher CFM than the intake system can handle. Essentially putting the air in faster than the engine can expell it?

    Is this the reasoning behind making the exhaust ports smooth and intake ports rough?
    Amongst other things I'm interested in how different bottlenecks in the intake system affect the air density ad it flows into the chamber. Like going from a 2.5"I/C piping to Some sloped endtanks with a large pressure drop then back to 2.5" piping...

    In my offhand experience, A/C systems use a similar pressure drop scenario to drop the temperature of the flow.
    If some of the physics transfer over would it make sense for me to have 2.5" IC piping to FMIC then 3" piping to a 3" TB and intake? Or will 99.9% of the cooling be from the FMIC as I suspect?
    Additionally it seems other people from my researching are bigger supporters of the larger turbo denser cooler air theory...

    Please let's not let this thread die just yet in the tech section. Personally never even been there lol

    Shane Drake
    Going to try to go question mark by question mark

    yes.

    The performance of a turbine is increased the more you decrease the pressure behind it. The lower the atmo, the more power to the turbine, and it will spin the compressor faster than it normally would be (reference your compressor maps). This moves it to a more advantageous area of the map. Unfortunately its input pressure is still lower due to altitude, and that loss carries through the entire system. These two effects have a give and take throughout speed ranges, but essentially equal out.

    Compressible as a term has nothing to do with pressure, only density. Read the text of the "isentropic flow" link. It has a pretty good textual description of why the density doesn't change.

    The turbine supplies power to the entire shaft and wheel system. Minus the aero and bearing drag, and divided by a rotational inertia, you get a compressor acceleration that results in a shaft speed. The shaft speed will flow what your cams will let in, and your boost pressure will be the dependent on all of that, and is given based on testing in the compressor map. It is very hard to calculate all these things accurately, but thats how it works in theory.

    No Idea, never heard of that, know very little of valve design or compressor aero.

    Increasing piping size will have a small loss (eddies and such) but will simply slow the velocity, not decrease the temperature. The intercooler produces a true temperature differential to drive the heat dissipation there.
    Last edited by Sprode; 10-10-2011 at 07:38 PM.

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    Veteran Member Four Rings bman005's Avatar
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    Really informative! Just tryin to take it all in. I've always known how turbos work generally but never got into a discussion about all this, good stuff

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    Updated with a third section, also edited the definition of CFM. Going to be cleaning up the first and second post, and adding to the third.
    -Shane Drake-
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    Veteran Member Four Rings DRAKLORE's Avatar
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    Please note: a lot of work has gone into this thread. as it done via my iPhone! 100% of my AZing is done on this device, so a lot of corrections and editing errors occur. That third section was a bitch because it was only viewable in plaintext or non copyable PDF. I would highly recommend reading the whole article as it is very informative :-)

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    http://www.grc.nasa.gov/WWW/k-12/airplane/ngnsim.html

    Had some fun with this last night. Might be fun for some.

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    that link is definitely above me... I need to read up on aviation engines. got any links for that?

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    Anyone have anything else to add? I guess it may be time to let this die lol :-(
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    Quote Originally Posted by CorneliusRox View Post
    that link is definitely above me... I need to read up on aviation engines. got any links for that?
    If you search around in this little nasa site, it has all kinds of reviews. just use the site navigation at the bottom of each page

  40. #40
    Veteran Member Four Rings DRAKLORE's Avatar
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    Since it seems this week we are being a technical little section instead of wheels/exhaust/best chip ect

    I will bring this back from ze dead and hopefully we can get some added insight :)
    -Shane Drake-
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