I feel that a "How to" section that gives baby steps on how to find your way around would be invaluable to all users. If you fall at the first hurdle it is really hard to keep going.
Simple things like the lack of a full list of what the parameters do is nothing short of unbelievable.
In the spirit of sharing, I wanted to show the steps I used to calculate the airflow through my turbos, it might help others struggling with the basics of using a Maths channel in SView.
I have an R35 GTR with a new engine build that I am working with and wanted to see if it was possible to work out the airflow through the Turbos to calculate where I am on the Compressor Map with a view to setting the maximum boost level.
I could not find any instructions on how to use the Maths function online, but turns out it is really easy and in my case very useful.
The principle I wanted to explore was that since the ECU delivers an injector duty cycle to maintain an air / fuel ratio, I should be able to calculate the flow of fuel and therefore it should be easy to calculate the flow of air.
Here is the result, the Orange line shows the air flow though one of the turbos through a 3rd and 4th gear pull

Here is the formula I used 14.7*lam2*sqrt(12.47267*relFp1/2999)*fuelDutyPri1/100*6/2
Here is the Math channel input screen in SView - Click Math > New and you can type it in

Here is the turbo compressor map on my car that shows it will deliver 60lbs of air /min.
The calculation shows I am at 50lb just now, so can safely increase the boost.

To help you understand the formula, it is effectively Air fuel ratio * current fuel consumption :-
= Air fuel ratio * injector flow * injector duty
Getting the units to match is the first challenge since the Compressor Maps are in lbs of air flow per minute.
I will describe each part of the formula so will hopefully not lose you.
14.7*lam2*sqrt(12.47267*relFp1/2999)*fuelDutyPri1/100*6/2
14.7*lam2 calculates the air fuel ratio from Lambda.
14.7*lam2*sqrt(12.47267*relFp1/2999)*fuelDutyPri1/100*6/2
sqrt(12.47267*relFp1/2999) calculates the flow through the injector for the current fuel pressure.
The formula I used is square root of new flow = old flow squared * new pressure / old pressure.
I have ID2000 injectors, they flow 2225cc/min at 43.5 psi, this is 3.531667 lbs of fuel per minute. The compressor map is in lbs air per minute, so the units are important.
12.47267 from the formula is 3.531667 squared, relFp1 is the differential fuel pressure (fuel pressure - boost) 2999 is the 43.5 psi in the Syvecs units, millibar or something like that.
14.7*lam2*sqrt(12.47267*relFp1/2999)*fuelDutyPri1/100*6/2
fuelDutyPri1 = injector duty
14.7*lam2*sqrt(12.47267*relFp1/2999)*fuelDutyPri1/100*6/2
100*6/2 = 100 takes the injector duty to a % when you want to multiply it. 6 = six injectors. 2 is because there are two turbos.
So, having done all that I am not sure how to save the Maths calculation so that it is permanently attached to the view I shared above.
Thanks
Hugh