When you talk turbos and engines, everything is computed by mass flow not volume. Volume is kind of a weird way to address it.
When your car measures intake temp, pressure, manifold pressure and manifold temp (and in some cases MAF)... it is really computing mass flow (I believe they used to call this a speed density system).
For non turbo flow mass flow = density * speed * area. You can solve in any way you want using Algebra.
The speed * area actually give you a volume/second. While the density gives you the mass flow of that volume.
Of course there isn't an easy way to measure density of moving air... so it is calculated by a number of sensors.
What is actually done (and much simplified for this discussion) is to consider the mass of air constant.
We then measure the mass of air coming in and record its temperature.
Then we calculate its energy with some more equations.
Then we add the fuel energy to it.
We then add the fuel mass and air mass and do some special math to figure out how they relate the pressure to temperature based on the chemistry of the burned mixture.
Then we subtract the power we extract from the crankshaft (including friction losses).
Then we expand the gas volume and divide by the ratio. This gives us the final pressure prior to opening the exhaust valve.
THEN we can calculate the density of the exhaust valve.
Once we do that we can figure out the speed of sound of the gas and calculate the maximum speed we can push it through the exhaust valve openings (which is exactly the speed of sound).
What is important to remember is that speed of sound is a function of density, pressure and temperature. Alter any of those and the speed of sound changes and thus the maximum flow rate through the exhaust.
You are correct in saying that the velocity drops as the gas contracts. However... piping size is really more a function of scavenging effects then anything. If you want scavenging in an exaust system you want a high velocity so the wake after the pressure pulse goes by creates a lower pressure then otherwise would be present.
So in general small tubes = fast velocity, large tubes = slow velocity and to an extent less energy.
The real tough part is picking the right size as the Mach number changes based on the pressure in the manifold. The Mach number sets the speed limit of the gas in the tube and therefore its flow rate. So when you hear people talk about hotter exhaust it is usually to give them a higher speed of sound, thus higher flow through the tube. But ALSO scavenging effects from higher velocity are important too.
In the turbine inlet there is a tapering shape that converts pressure energy into velocity energy by reducing the area. This is called a nozzle. It is basically a funnel.
The less area you have the higher the velocity is up until the speed through the smalls area of the nozzle is Mach 1 (at whatever the Mach value is for the gas at that point).
Interestingly enough a you can only move so much air so fast through a nozzle before it refuses to move more air through with more pressure. So what this means is that there is a maximum flow rate through the turbo. The only way to increase this is to increase the exhaust pressure when the area is further reduced. This is where my discussion of efficiency comes in. As the increased exhaust pressure needed to push the air through the nozzle faster causes an increase on exhaust pressure which eventually means a tougher time moving air in and out of the cylinder. At some point the turbo is pushing air just to overcome the exhaust pressure requirements. This decreases the output power unless sufficient additional air and fuel are thrown into the cylinder.
You are somewhat right with the diameters... except we area really talking about velocity to the turbine wheel and flow. With flow comes the exhaust energy that the turbine wheel removes and uses to power the compressor wheel.
Turbine wheels don't make a lot of torque, but they do turn at several hundred thousand RPM. What this means is that using the above formula HP=torque*RPM/525 you can estimate the turbine torque. Say the compressor puts out 40 HP worth of air compressing at 170,000 RPM. You can see that the torque is 1.23 ftlbs. The turbine wheel spins faster for higher velocity and slower for slower velocities. For the most part the turbine extracts more power at higher RPMs with more exhaust energy.
Turbo size is effected by the max flow. A big turbo requires a lot of mass flow and energy to spin, while a small turbo requires less and there fore produces less compressor power...
The differences is one will max out sooner than the other.
Interestingly enough in the 800-1000 HP engine classes the turbos area almost always about the same size whether you are talking about a small 4 cylinder drag engine or a large 550 CI big block. The difference really comes down to how much air each engine flows and how much it takes to power the turbo up.
In fact I'd be willing to bet in a competition drag 4 cylinder that the turbo spools itself up as it delivers more and more air to the engine. Which would give it a slower lag time then the bigger 550 CI... which based on mass flow could spool it up at a much lower engine RPM....
Hope this makes some sense. Any other thoughts?
When your car measures intake temp, pressure, manifold pressure and manifold temp (and in some cases MAF)... it is really computing mass flow (I believe they used to call this a speed density system).
For non turbo flow mass flow = density * speed * area. You can solve in any way you want using Algebra.
The speed * area actually give you a volume/second. While the density gives you the mass flow of that volume.
Of course there isn't an easy way to measure density of moving air... so it is calculated by a number of sensors.
What is actually done (and much simplified for this discussion) is to consider the mass of air constant.
We then measure the mass of air coming in and record its temperature.
Then we calculate its energy with some more equations.
Then we add the fuel energy to it.
We then add the fuel mass and air mass and do some special math to figure out how they relate the pressure to temperature based on the chemistry of the burned mixture.
Then we subtract the power we extract from the crankshaft (including friction losses).
Then we expand the gas volume and divide by the ratio. This gives us the final pressure prior to opening the exhaust valve.
THEN we can calculate the density of the exhaust valve.
Once we do that we can figure out the speed of sound of the gas and calculate the maximum speed we can push it through the exhaust valve openings (which is exactly the speed of sound).
What is important to remember is that speed of sound is a function of density, pressure and temperature. Alter any of those and the speed of sound changes and thus the maximum flow rate through the exhaust.
You are correct in saying that the velocity drops as the gas contracts. However... piping size is really more a function of scavenging effects then anything. If you want scavenging in an exaust system you want a high velocity so the wake after the pressure pulse goes by creates a lower pressure then otherwise would be present.
So in general small tubes = fast velocity, large tubes = slow velocity and to an extent less energy.
The real tough part is picking the right size as the Mach number changes based on the pressure in the manifold. The Mach number sets the speed limit of the gas in the tube and therefore its flow rate. So when you hear people talk about hotter exhaust it is usually to give them a higher speed of sound, thus higher flow through the tube. But ALSO scavenging effects from higher velocity are important too.
In the turbine inlet there is a tapering shape that converts pressure energy into velocity energy by reducing the area. This is called a nozzle. It is basically a funnel.
The less area you have the higher the velocity is up until the speed through the smalls area of the nozzle is Mach 1 (at whatever the Mach value is for the gas at that point).
Interestingly enough a you can only move so much air so fast through a nozzle before it refuses to move more air through with more pressure. So what this means is that there is a maximum flow rate through the turbo. The only way to increase this is to increase the exhaust pressure when the area is further reduced. This is where my discussion of efficiency comes in. As the increased exhaust pressure needed to push the air through the nozzle faster causes an increase on exhaust pressure which eventually means a tougher time moving air in and out of the cylinder. At some point the turbo is pushing air just to overcome the exhaust pressure requirements. This decreases the output power unless sufficient additional air and fuel are thrown into the cylinder.
You are somewhat right with the diameters... except we area really talking about velocity to the turbine wheel and flow. With flow comes the exhaust energy that the turbine wheel removes and uses to power the compressor wheel.
Turbine wheels don't make a lot of torque, but they do turn at several hundred thousand RPM. What this means is that using the above formula HP=torque*RPM/525 you can estimate the turbine torque. Say the compressor puts out 40 HP worth of air compressing at 170,000 RPM. You can see that the torque is 1.23 ftlbs. The turbine wheel spins faster for higher velocity and slower for slower velocities. For the most part the turbine extracts more power at higher RPMs with more exhaust energy.
Turbo size is effected by the max flow. A big turbo requires a lot of mass flow and energy to spin, while a small turbo requires less and there fore produces less compressor power...
The differences is one will max out sooner than the other.
Interestingly enough in the 800-1000 HP engine classes the turbos area almost always about the same size whether you are talking about a small 4 cylinder drag engine or a large 550 CI big block. The difference really comes down to how much air each engine flows and how much it takes to power the turbo up.
In fact I'd be willing to bet in a competition drag 4 cylinder that the turbo spools itself up as it delivers more and more air to the engine. Which would give it a slower lag time then the bigger 550 CI... which based on mass flow could spool it up at a much lower engine RPM....
Hope this makes some sense. Any other thoughts?
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