Ok, here comes more.
Spit I, 1939, 87, Merlin III, Rotol CS.
Climb to 10K in 3.5 mins and to 20K in 7.7
That gives respectively 2372464286N/sec to 10 K and 2156785714N/sec to 20K
Move to the Merlin XII and with a weightier aircraft, 100 oct+rotol, you go to 3.35 to 10K, and straight 7 to 20K
I belive these are 1939 figures (will someone check?) so there already seem to be some stock of 100 grade fuel.
That gives respectively 2528677612 N/sec to 10K and 2420305714 N/sec to 20K
NOTE! These are rather good Spitties, the 2 bladed ones are vastly worse.
A nice little 109 I found gave 3.7 and 8 minutes to 10 and 20K running on 87 octs,
Over to Newtons/sec, we have 2179307432 and 2015859375.
So, with almost exactly the same HP, a Spit I once it has the rotol CREATES some 5-8% more lift than it's contemporary with what most clame to be about the same power. Interesting.
(BTW, a 109E-3, 1940, weight 5875 lbs, rated at 1050 hp)
AFAIK the 100 grade was not used by the BEF in France, but entered early in the BoB.
Anyway, the 3-bladed propeller changed more in the climb rate than the conversion to 100 octs.
So, with both, you are looking into the second number which gives created lift with more than 15% between the contemporaries.
But the Spitfire is heavier, - actual time difference to alt is some 4% and 12%.
So, that was Spitties climb rate to 10K and 20K with 87 oct and 100 oct on CS.
Always on the hunt for Emil tests though.