Tony, you posted under Chris again.
JK I am sure Chris has made compressor maps, probably at his day job.
Perhaps you can share some of the ones you made?
What turbos did you make them for and why go through the hassle?
What would you guesstimate GCs flow lb/min?
We agree on one thing, an engine is an air pump!
Compressor maps made were for turbine engines, proprietary stuff that I can't share, but I can say the engines I've done testing for are on many planes that you've probably had flights on (Boeing, some of the big Airbus) and more often they're on planes that you probably haven't had rides on (but maybe) such as the nice Gulfstream business jets, and some that I hope you haven't had to have rides on (secret). In this case it's important to be able to define the flight envelope for starting, operability, and performance (how high, hot hot, how cold, how much load, what type of load, etc). It's extremely similar to turbos, which is why there is so much transference between the two careers. In fact, take your compressor output, feed it into the turbine inlet, add some fuel and a flame source and you'll make your own turbine engine. Few youtube vids of some brave individuals doing such a thing.
Some of these guys have no clue how close death is. *shudder*
Mapping is a large scale effort, often testing is accomplished in an environmental chamber that simultaneously controls air temp, conditioning, and density for the chamber independent of what we're feeding the motor (allows us to replicate weird scenarios such as being up at 40kft, having everything soaked to -65F for hours, then needing to start during the descent or landing on a hot day, so motor is cold soaked, altitude is whatever we want, inlet temperature is hot day). Standard engineering approach, stack the odds in every which way until you've tested every conceivable possible iteration that is possible in flight. The compressors we use for the test chamber control are beyond enormous, 3500 horsepower or so, which is so large in fact that we're prohibited from running full scale during the day, as the electrical demands are so significant. It's expensive too, the better part of 20k/day to run one of these tests, there is no such thing as a test that's less than 6 digits and often pushes well into 7.
Why do a compressor map for a turbo? It's a good question. I'm not sure it's worth the hassle for what we're doing here, although it would allow you to no-shit understand the flow differences between blade iterations and you'd see the edge (surge or stall) long before you got there, as well as understand how that particular design behaves near that edge. Our flow and performance guys are among the best on this earth and they'll freely admit no computer program (yet) is capable of analyzing all the data such that we can do it via analysis vs. test, which is one of the reasons I love testing so much, and also a reason I've enjoyed working with Tony. You're not going to find him doing CFD on a new blade design, but he's so aggressive with procuring, testing, and categorizing performance that I am impressed, and at the end of the day how she performs on the street is what matters to most of us. Anyway, we make these maps to understand both incremental and significant changes. The aviation industry often qualifies parts through similarity, but it can become a runaway train. Minor tweak to a compressor, no re-qualification testing needed. Minor combustor tweak, no test needed. Minor turbine blade tweak for manufacturability, we should be good there everyone agrees. Oh, fuel control vendor went tits up, let's cost reduce her a bit, qualify it on a component level and we're good. 10 years later you've really lost your footing on what the limits are, and when cert requirements change, and customers don't want it qualified to the old standard you've been claiming similarity to, at some point you have to own up that you prob need to revisit all the stuff, if for nothing else than making models that reflect real-world performance to help further design iterations. I've wandered a little bit, this field is something I spend most of my time working on. Bottom line is a compressor map shows the capability of that particular compressor, and will help you avoid some issues once in service.
Arguments against it are cost & effort first & foremost. Additionally a compressor map is still completely de-coupled from the system it's in. I.e. that's the compressor.... with what turbine? In what housing? At what temperature, altitude, etc? Once in the car, with what inlets, what outlets, FMIC, charge pipe, throttle, head, valves, etc? All of this impacts the delta P across the compressor (among a million other things), so I tend to view compressor maps as more a tool of comparing compressor to compressor (i.e. advanced blade designs) versus suitability for a particular application -too many other variables in turbo design that will make it sink or swim.
Once you have some experience goofing around on a motor, you can glean rough power potential from a compressor map, if you assume the rest of the system isn't completely stupidly designed (usually.... but not always). The N54 is efficient at turning flow into whp. An estimate on GC v2.0 capability would just be backwards calculated from our testing, which would lead you to somewhere around 40lb/min, but this is just shit kicking talk, nothing authoritative. Tony actually may have a better idea. I'll say this, there are PLENTY of gains to be had by flow-optimizing the system; all of us are paying the penalty of envelope compromises. I.e. the stuff has gotta fit in the space we have, optimized flow be damned.
That's enough wandering for a Sunday morning. I'm going to have more coffee and chase the wife around.
Chris