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After some research concerning those aircraft that were decidedly subsonic
in level flight (no pushover from altitude to gain greater speed), it would appear mach effect is the overriding concern. The last low altitude record before the transition to high (F-100, with several ... F-86, F-4D ... previous to that) were all done at the Salton Sea. Hi temp (higher TAS for mach) and low altitude (-227 MSL), delayed transonic drag rise. The PsubS bulge doesn't occur until you get into the cleraly supersonic designs. Then it behooves a "low altitude" record to occur as high above MSL as possible. Hence the sageburner and later Greenamyer efforts in the high desert (less IAS, more TAS, 988 mph for Darryl ... great film by the way). Bottom line, in our running discussion, I now find your argument compelling. I was incorrect. R / John |
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