Yap, ditto :) There is a great R-35 engine chart, both altitude-thrust and Mach-thrust related. I have entered it for the Flogger(s) for 0-24 km altitudes in one km increments. It seems that it behaves just a little below norm, but Mach table (in my 1st post) is off by cca. 200% (rather that initially estimated 100%).
This is from the sheet:
WetMachTableNumData=7 (no.of entries)
WetMachTableDeltaX=0.4 (M0.4 increments)
WetMachTableStartX=0.0 (staring from M0)
WetMachTableData=1.000,0.960,1.250,1.500,1.330,1.160,1.083 (thrust multiplier at M0, M0.4, M0.8, M1.2, M1.6, M2.0, M2.4). This gives 18-19000kgf thrust in real engine at ceiling (M.1.6).
The last number for "stock" Phantoms is over 3! When "default" table is put, Floggers can do something over 10,000m. Else engines "die" in the air too poor but too thick. Maybe TK made Nytrogen atmosphere? ;)
As in the Thirdwire-StreakEagle's mod for J79, "altitudetablenumdata" of R-35 in manual is a little "thinner" above 9-10,000m. I suppose StreakEagle took his from a manual, too (only he did cut it a bit fine, 91 300m-steps to cca 21,000m and I did it in 1000msteps to 24km)!
In overall, I think that wetmachtable is the one that needs "corrective factor" starting from cca. M1. For values above M1 I entered "default" correction, and it behaves more-less ok, but it would good to know the real "offset behaviour".