Very well done. Gas turbine engine is my area of 'expertise', and I have to say that this text is very well written, with many details showing how things work, but yet, it's simple enough for the general public to understand. :) By the way, the TF30 doesn't have a hyphen between TF and 30 :D (little detail LOL).
Here's a bit more information about the F110-GE-400 engines:
Length − Overall: 232 inches
Nominal Diameter: 45.5 inches
Max Radial Projection: 52 inches
Weight, Dry: 4494 lbs
Weight, Wet: 4592 lbs
MAX THRUST: 26,950 RPM: 14,666 (HPC) 8,257 (LPC) SFC: 2,104 AIRFLOW: 261 lbs/s
MAX CONTINUOU THRUST: 14,696 RPM: 14,459 (HPC) 8,038 (LPC) SFC: 0,576 AIRFLOW: 245 lbs/s
So a quick math shows that the engine at sea level, standard day conditions has a fuel flow of 56,702 pounds in an hour in AB. MAX CONTINUOUS having a Fuel flow (FF) of 8,622.
At an altitude of 35,000 at Mach 1.6 the -400 engine produces around 20,966 lbf and has an S.F.C of 2.261, airflow is 268 lbs/s.
Thanks for the update!