Easy, follow Supermarine's lead with dedicated LF HF models for optimal performance.but how do you get a plane to perform well at both say sea level to 5000 ft vs 30,000 ft?
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Easy, follow Supermarine's lead with dedicated LF HF models for optimal performance.but how do you get a plane to perform well at both say sea level to 5000 ft vs 30,000 ft?
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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.
I'm not too sure a 1949 P-51H would do very well in a 1944 - 1945 fight.
The P-51H made WWII Wayne. I'm sure you know that. Didn't make it into combat, but made the war. Ditto the F8F.They made P-51Hs in 1949, or merely ran tests in 1949?
Firstly what is "high altitude? In 1940 Spitfires and Hurricanes struggled to intercept at 30,000ft. By 1942 with the Ju 86 being used they had to get up to circa 42,000 . You cannot disregard the laws of physics. Spitfires modified to get to those altitudes were compromised lower down, the extended wing tips lowered rate of roll and made them float on landing, while removing the radio and armour took them back to the bi plane era.