Dynamic Airflow ?
Last edited by Silverhawk_02TA; Apr 26, 2005 at 04:46 PM.
I went back to look at some old WOT logs, and here is what I found: at WOT, as the RPM's go up, MAP is steadily dropping. However, Dynamic Cylinder Air (and hence airflow overall) is steadily climbing. This shows that the amount of airflow is not directly proportional to MAP. We can see how this is possible if we look at the mass flow equation:
Mass flow = (VE * MAP * RPM * Displacement) / IAT
So, the MAP may be dropping, but the RPM is climbing. Displacement of course is not changing.
So, in your case GMCVT, not only is your MAP dropping, but also your Dynamic Cylinder Air. This may indeed be due to the restrictiveness of the stock intake path. However, keep in mind that the equation for mass flow (from which Dynamic Cylinder Air is derived) is also dependent on the VE table. If you have not tuned the WOT cells on your VE table, then you can take those Dynamic Cylinder Air values and throw them out the window right now. Have you tuned those WOT, high RPM VE cells?
I went back to look at some old WOT logs, and here is what I found: at WOT, as the RPM's go up, MAP is steadily dropping. However, Dynamic Cylinder Air (and hence airflow overall) is steadily climbing. This shows that the amount of airflow is not directly proportional to MAP. We can see how this is possible if we look at the mass flow equation:
Mass flow = (VE * MAP * RPM * Displacement) / IAT
So, the MAP may be dropping, but the RPM is climbing. Displacement of course is not changing.
So, in your case GMCVT, not only is your MAP dropping, but also your Dynamic Cylinder Air. This may indeed be due to the restrictiveness of the stock intake path. However, keep in mind that the equation for mass flow (from which Dynamic Cylinder Air is derived) is also dependent on the VE table. If you have not tuned the WOT cells on your VE table, then you can take those Dynamic Cylinder Air values and throw them out the window right now. Have you tuned those WOT, high RPM VE cells?
Your trims go to 0 at WOT because the PCM is going into PE mode.
At constant throttle (constant orifice) as the RPMs increase there is an increased airflow through the throttle/orifice and a vacuum does develope - relative to atmospheric pressure. So, if atm is ~ 101.4 kPa then it will drop towards 20 kPa.
Volumetric Efficiency tables drop after Peak Torque, typically (NA). Actually it's the VE creating that Torque. HP continues upward due to increasing RPMs.
Here's an excellent overview (from an aviation author ...highly applicable tho) of the internal combustion engine and performance ->>
http://www.eaa1000.av.org/technicl/engemp/engemp1.htm
Hope this helps some.
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Your trims go to 0 at WOT because the PCM is going into PE mode.
So let me see if I have this right. I obviously do not have my PE disabled, so at WOT the PCM is looking at the PE table. If thats the case then how does that then affect the validity of the Dynamic cylinder airflow? Thank you again and sorry for the ignorance. Last edited by GMCVT; Apr 26, 2005 at 09:09 PM.
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Your trims go to 0 at WOT because the PCM is going into PE mode.
Maybe newb question, but how do you disable PE mode (new HPT User)?
and
I assume when the PE is disabled, most engines will be leaner than desired, so how does the VE tuning accomplish the desired AFR? If you could explain, here or email me about it, sounds like something I would be interested in doing. Also, assuming I !PE, tune with VE tuning guidelines, would I be able to acheive a richer>Max Tq and then leaner>from Max TQ to Max HP AFR using a wideband for input? And finally, once it is dialed in, go back and adjust the PE for 1.00 meaning not to add anything, or 1.xxx to give me a richer package for a separate nitrous tune?
Thanks
Charlie
At constant throttle (constant orifice) as the RPMs increase there is an increased airflow through the throttle/orifice and a vacuum does develope - relative to atmospheric pressure. So, if atm is ~ 101.4 kPa then it will drop towards 20 kPa.
Volumetric Efficiency tables drop after Peak Torque, typically (NA). Actually it's the VE creating that Torque. HP continues upward due to increasing RPMs.
Here's an excellent overview (from an aviation author ...highly applicable tho) of the internal combustion engine and performance ->>
http://www.eaa1000.av.org/technicl/engemp/engemp1.htm
Hope this helps some.
and
I assume when the PE is disabled, most engines will be leaner than desired, so how does the VE tuning accomplish the desired AFR? If you could explain, here or email me about it, sounds like something I would be interested in doing. Also, assuming I !PE, tune with VE tuning guidelines, would I be able to acheive a richer>Max Tq and then leaner>from Max TQ to Max HP AFR using a wideband for input? And finally, once it is dialed in, go back and adjust the PE for 1.00 meaning not to add anything, or 1.xxx to give me a richer package for a separate nitrous tune?
Also, keep in mind that DCA is a calculated and not measured value, so it's only as good as the data going in. If your VE values are incorrect, your DCA values don't mean squat. It being a calculated and not measured value also means that it cannot be used in and of itself to show the efficiency of the intake/exhaust regardless. It's the VE table which does this.
The only reason I disable PE is so I can tune the cells in the VE table close to and including WOT using fuel trims. If I didn't do this, PE mode would kick in when I hit those cells and skew my fuel trims. Once I finished that, I re-enabled PE mode. After using this method to tune my WOT VE values, I can command a solid AFR in the PE table, and all my O2 readings are within .005 mv of eachother during a logged WOT run, which shows that my VE values are dead on.
VE is representative of the TQ curve, but not necessarily DCA. As Bink said, VE tends to be max where the TQ peak is, and fall off after that. My max VE is 101 at 5200 RPM (my TQ peak) and drops off to 97 at 6200 RPM, where my rev limiter is set at. After my TQ peak, both my VE and MAP are falling, but my DCA is still going up. Looking at the mass flow equation, VE and RPM are their raw values, and MAP is in bars. As such, the mass flow output of the equation is most heavily affected by RPM, since both VE and MAP are much smaller numbers. Hence, as long as RPM is rising, only VE and/or MAP falling off considerably should cause a decrease in DCA. My DCA at 5200 RPM is .68 g/cyl, while at 6200 RPM it's at .70 g/cyl, despite my VE dropping from 101 to 97, and my MAP dropping from 83 to 81 kpa. If I logged up past 6200 RPM, my VE and MAP would probably fall to the point that my DCA would start dropping before I hit 7000 RPM.
Also, keep in mind that DCA is a calculated and not measured value, so it's only as good as the data going in. If your VE values are incorrect, your DCA values don't mean squat. It being a calculated and not measured value also means that it cannot be used in and of itself to show the efficiency of the intake/exhaust regardless. It's the VE table which does this.


