Just installed md isothermal manifold gasket, ccv.
Originally Posted by Hydrazine
The air isn't in the plenum for too long, but the transfer rate is much higher in that area than it is in the intake tube for example. Because the flow in the runners is pulsed/oscilating flow, it has a way of scrubbing the hot boundary layer right off the plenum. The air flow in there is very turbulent.
Originally Posted by Hydrazine
When the engine is running and the plenum is in thermal equilibrium, the heat transfering through the lower plenum is equal to the heat transfering into the air.
Originally Posted by Hydrazine
Because we know the air flow rate (can be found), and the heat capasity of air is known. We can calculate the rise in temperature of the air.
The only problem is, I havn't done the calculation yet.
Its not hard, it will just take a little time to gather all the variables and constants.
I could either do that or just put thermocouples in the flow stream of one of the runners and be done with it.
The only problem is, I havn't done the calculation yet.
I could either do that or just put thermocouples in the flow stream of one of the runners and be done with it.
I would assume the flow transitions from a laminar to a turbulent boundary layer at some given rpm
If this were steady state flow that would clearly be the case. But with pulsed flow where the air is oscilating (bouncing back and forth) it gets turbulated really quick. Each of the intake runners is humming as a 1/4 wave resonator or like a Coke bottle with air blown across the top of it. The osscilation scrubs away boundary layers and any insulating action they may offer. That is why heat reduction in the plenum is much more important than in the air tube where the flow is more continuous.
Won't the air flow be insulated by the tubulent boundary layer so the temperature of the air flow will never be the same temperature as the plenum?
No. Turbulation does the opposite. It increases the heat transfer rate by orders of magnitude. Laminar boundary layers do the insulating.
I understand there will be heat transfer, but at a reduced rate as compared with the heat transfer between the plenum and the boundary layer?
With or without Iso Thermal, the boundary layer (or a lack of it) will be the same for either configuration.
I am very interested in these comments to learn more about the heat transfer rate......I have access to Fluent, which I might be able to use on a limited basis. But I would need help with the problem definition and the boundary conditions.......
Fluent can calculate the boundary conditions for you, but modeling the plenum and intake runners into Fluent would be a real programming challenge.
If this were steady state flow that would clearly be the case. But with pulsed flow where the air is oscilating (bouncing back and forth) it gets turbulated really quick. Each of the intake runners is humming as a 1/4 wave resonator or like a Coke bottle with air blown across the top of it. The osscilation scrubs away boundary layers and any insulating action they may offer. That is why heat reduction in the plenum is much more important than in the air tube where the flow is more continuous.
Won't the air flow be insulated by the tubulent boundary layer so the temperature of the air flow will never be the same temperature as the plenum?
No. Turbulation does the opposite. It increases the heat transfer rate by orders of magnitude. Laminar boundary layers do the insulating.
I understand there will be heat transfer, but at a reduced rate as compared with the heat transfer between the plenum and the boundary layer?
With or without Iso Thermal, the boundary layer (or a lack of it) will be the same for either configuration.
I am very interested in these comments to learn more about the heat transfer rate......I have access to Fluent, which I might be able to use on a limited basis. But I would need help with the problem definition and the boundary conditions.......
Fluent can calculate the boundary conditions for you, but modeling the plenum and intake runners into Fluent would be a real programming challenge.
Originally Posted by Hydrazine
If this were steady state flow that would clearly be the case. But with pulsed flow where the air is oscilating (bouncing back and forth) it gets turbulated really quick. Each of the intake runners is humming as a 1/4 wave resonator or like a Coke bottle with air blown across the top of it. The osscilation scrubs away boundary layers and any insulating action they may offer. That is why heat reduction in the plenum is much more important than in the air tube where the flow is more continuous..
Originally Posted by Hydrazine
Turbulation does the opposite. It increases the heat transfer rate by orders of magnitude. Laminar boundary layers do the insulating.
Originally Posted by Hydrazine
With or without Iso Thermal, the boundary layer (or a lack of it) will be the same for either configuration.
Originally Posted by Hydrazine
Fluent can calculate the boundary conditions for you, but modeling the plenum and intake runners into Fluent would be a real programming challenge.
Thanks Shooter
Originally Posted by shooter82
I was thinking of analyzing a much simplier problem to start with......a simple box with 7 holes, one inlet and 6 outlet.......and apply the G boundary conditions.......I was looking for an estimate for the mass flow rate and plenum temperature. I could vary either or both of these parameters. Do you feel this would be a worthwhile endevour?
Thanks Shooter
Thanks Shooter
It will probably be a lot easier and more accurate to simply run a test with the Innovate Motorsport box streaming the data. I will put thermocouples into the flow stream to find the answer.
it only took me 12 years but I finally bought one of these gaskets yesterday lol.
plus...
This thread (and forum) deserves a thread bump for useful "heritage" items like this.
plus...
This thread (and forum) deserves a thread bump for useful "heritage" items like this.
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