I just cannot forsee these massive air to air units we've seen conjectured in early renderings taking up an entire sidepod making sense. One sidepod for an intercooler, and the other for a traditional radiator? I can't see it.

Right you are. I was only making it clear, that on low boost systems, there's not much difficulty in running without an intercooler, because someone claimed it was very difficult to run a turbo without an intercooler.ringo wrote:You can't have a fuel limited racing series and then have a turbo charged engine without an intercooler.
The intercooler directly affects the fuel efficiency of the engine. I think we had this discussion in the engine thread.
An intercooler, even a really small one would still most likely be wider than the turbo air inlet required for next year so it will just be disturbing airflow to the rear wing. And seeing as rear down force wont be in abundance next year I find this solution highly unlikely.Ferraripilot wrote:A mini intercooler just behind the driver's head or between the fuel tank partially in the path of the intake flow could make sense. Coolant from the traditional radiator system could be shared with the liquid to air intercooler perhaps with all coolant filter in through the intercooler first prior to entering the engine.
I just cannot forsee these massive air to air units we've seen conjectured in early renderings taking up an entire sidepod making sense. One sidepod for an intercooler, and the other for a traditional radiator? I can't see it.
RicerDude wrote:
An intercooler, even a really small one would still most likely be wider than the turbo air inlet required for next year so it will just be disturbing airflow to the rear wing. And seeing as rear down force wont be in abundance next year I find this solution highly unlikely.
Yes, that is true. But it is slightly different with piston engines (otto cycle), since the extra heat can cause problems for combustion.timbo wrote:Here's paper on intercoolers in gas turbine (Brayton Cycle) it actually says intercoolers hurt thermal efficiency:
http://web.me.unr.edu/me372/Spring2001/ ... ration.pdf
Agreed, but without the limit of ON in fuel, and high pressure multi-phase injection is it a problem that can be solved I wonder?wuzak wrote:Yes, that is true. But it is slightly different with piston engines (otto cycle), since the extra heat can cause problems for combustion.timbo wrote:Here's paper on intercoolers in gas turbine (Brayton Cycle) it actually says intercoolers hurt thermal efficiency:
http://web.me.unr.edu/me372/Spring2001/ ... ration.pdf
Not exactly. Depends on where the intercooler is placed.timbo wrote:Here's paper on intercoolers in gas turbine (Brayton Cycle) it actually says intercoolers hurt thermal efficiency:
http://web.me.unr.edu/me372/Spring2001/ ... ration.pdf
The intercooler reduces the temperature of the air exiting the compressor and entering the combustion chambers. That means lower temperature on the entry to the turbine, which means lower thermal efficiency.ringo wrote:Not exactly. Depends on where the intercooler is placed.timbo wrote:Here's paper on intercoolers in gas turbine (Brayton Cycle) it actually says intercoolers hurt thermal efficiency:
http://web.me.unr.edu/me372/Spring2001/ ... ration.pdf
It's not black and white. The compression work is reduced, not the thermal efficiency.
It can be shown thermodynamically why intercooling between compression stages increase efficiency.
You have interpreted the documented incorrectly.
The intercooler reduces the temperature of the air exiting the compressor and entering the combustion chambers. That means lower temperature on the entry to the turbine, which means lower thermal efficiency.ringo wrote:Not exactly. Depends on where the intercooler is placed.timbo wrote:Here's paper on intercoolers in gas turbine (Brayton Cycle) it actually says intercoolers hurt thermal efficiency:
http://web.me.unr.edu/me372/Spring2001/ ... ration.pdf
It's not black and white. The compression work is reduced, not the thermal efficiency.
It can be shown thermodynamically why intercooling between compression stages increase efficiency.
You have interpreted the documented incorrectly.
No an intercooler is not before a turbine. It is always between compression stages.wuzak wrote:
The intercooler reduces the temperature of the air exiting the compressor and entering the combustion chambers. That means lower temperature on the entry to the turbine, which means lower thermal efficiency.
Nope. I've done some turbo machinery theory many years ago, reheat is not for recovery. It's simply to raise the pre combustion temperatures. You can still use reheat on a system with no intercooler.This can be recovered by using reheat - burning a little more fuel in the exhaust and running it through a second turbine.
What higher temperature does is reduce the amount of heat needed to be added by the fuel.And/Or regeneration. Regeneration is taking the waste heat from the exhaust and using it to increase the air temperature after the compressor. This results in higher temperatures at the turbine or less fuel required to reach the same temperature.
You are trying to back out of the discussion now by muddling the discussion. Why are talking about efficiency of the turbine, when you were orginally talking about thermal efficiency?Intercooling between compressor sets (high and low pressure, rather than every individual stage) does lower the compressor work required, but does not increase the overall efficiency of the turbine.
Let me reveal a secret to you.It is also irrelevent for most reciprocating turbo engines. Intercooling in turbo engines really is aftercoling, since in most cases there is only one stage of compression. It is added to keep the intake air at a temperature that won't induce detonation in the engine.
This is so wrong. Compressing cooler air requires less work, just get back to your TD text books, you've got your channels crossed - time for a concept review.wuzak wrote:The intercooler reduces the temperature of the air exiting the compressor and entering the combustion chambers. That means lower temperature on the entry to the turbine, which means lower thermal efficiency.ringo wrote:Not exactly. Depends on where the intercooler is placed.timbo wrote:Here's paper on intercoolers in gas turbine (Brayton Cycle) it actually says intercoolers hurt thermal efficiency:
http://web.me.unr.edu/me372/Spring2001/ ... ration.pdf
It's not black and white. The compression work is reduced, not the thermal efficiency.
It can be shown thermodynamically why intercooling between compression stages increase efficiency.
You have interpreted the documented incorrectly.