re
It is interesting. The chart you link to above for the P-51H is from 18 December 1944 (so a prototype or pre-production airframe) running at 70"Hg without ADI at 9530 lbs TOGW (with? without? DT/bomb racks), and the ACA Vmax altitudes (31,500/17,500 ft) are considerably higher than for the later F-51H SAC chart I posted above, which is from 1949 running at 80" with ADI at a Combat weight of 9430 lbs with DT/bomb racks. So the 1949 F-51H is running with significantly more power at a 100 lb lighter weight, with ACA Vmax at considerably lower altitudes (22,700/9,000 ft) than the 1944 P-51H.