I think I see where he got his info and he's not wrong, but he's not completely right either. It might just be a matter of semantics. Interesting
topic though. I've spent a lifetime around aviation engines but have certainly never thought about this topic this much. My opinion on whether
"real world" experience or considered research is more valuable differs from yours however, as I've met plenty of mechanics everywhere from
Jiffy Lube to aviation engine test facilities who will repeat misinformation for decades. Best case scenario, there's research and application
involved.
Gasoline FAQ - Part 3 of 4
One of many pertinent sections here:
"The actual ignition timing to achieve the maximum pressure from normal combustion of gasoline will depend mainly on the speed of the engine and the flame propagation rates in the engine. Knock increases the rate of the pressure rise, thus superimposing additional pressure on the normal combustion pressure rise. The knock actually rapidly resonates around the chamber, creating a series of abnormal sharp spikes on the pressure diagram. The normal flame speed is fairly consistent for most gasoline HCs, regardless of octane rating, but the flame speed is affected by stoichiometry. Note that the flame speeds in this FAQ are not the actual engine flame speeds. A 12:1 CR gasoline engine at 1500 rpm would have a flame speed of about 16.5 m/s, and a similar hydrogen engine yields 48.3 m/s, but such engine flame speeds are also very dependent on stoichiometry."
Between this and other parts of the white paper, in plain words it comes down to premium gas
burning in a more controlled fashion, but under normal circumstances it burns neither slower nor quicker
than regular. What the premium additives do however, is prevent the flame from accelerating under higher
pressures and pressure spikes. So "premium burns slower" really means its burn rate is prevented from accelerating
under the pressure and pressure anomalies of very high compression. At least that's how I'm reading it.