Geoffrey Sinclair
Staff Sergeant
- 927
- Sep 30, 2021
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The 4lb boost was testing done using 87 Octane fuel, and that accounts for the increase in speed at 9lb boost. The FTH of the Merlin VIII was only 2400ft at 9lb boost:In some "what if's" there may things just could not be done. Sticking an R-2800 in a Wildcat was not going to work.
Then there are some "what if's" that require time travel.
Then there are some "what if's" that were possible but were not done because they didn't think of it at the time. Dr. Sanford Moss of turbo-charger fame was asked why didn't they stick a combustion chamber in-between the compress and the Turbine of a turbocharger to make a small jet engine. He is supposed to have replied "dumb, just dumb". They already had 2/3rds of jet engine.
Building a folding wing Hurricane seems to certainly be possible. No reason it could not be done. And the Hurricane, while not ideal, was certainly better than some other candidates from around the world. The 10 out of 10 successful landing by RAF pilots in their first attempt at carrier landing with no hooks certainly points to the Hurricane having few problems.
But this was in June of 1940, a little late to cancel the Fulmar program. Experiments could have bee done earlier.
The arguments seem to be if the Hurricane could do the intended job/s and that means all of them, not just defending carrier/fleet over the carrier/fleet.
Part of this is the navigation question. British actually had a pretty good system. Seems to be better than the US and Japanese in 1939/40. What the Americans could or could not do in 1942 or 1944 does not have a lot of bearing on what the British could do/buy/make in 1939/40. We are starting to get into time travel.
The Hurricane didn't have the desired range/endurance. Which was solved later with drop tanks, could have been solved in the early 30s or even sooner. However carriers, especially small ones, don't have a lot of storage space. If you are carrying several hundred empty drop tanks what else did you leave home to make space?
And for some reason (dumb?) the British were fooling around with fixed external tanks, not drop tanks, for the Spitfire in 1939/40. Sticking fixed tanks on a Hurricane reduces the margin of performance over the Fulmar.
We have a fuel question, When did the RN know they were going to get 100 octane on their carriers. Not when did they get it, when did they know so they could make plans (order planes that could use it, like a year or more earlier).
A Fulmar at low altitude could do 216mph at 1000ft but the account says that was using 4lbs of boost which does not seem right (typo? or 2 typos?) A different plane was tested using 9lbs of boost (100 octane) and did 250mph at 1000ft and 255.5mph at 2400ft which seems unbelievable. Hurricane I gained about 20mph going from 6lbs of boost to 12lbs of boost.
Hurricane I (land plane) did about 265-270mph at 1000-2000ft using 6lbs and a CS prop. Did around 290mph using 12lbs of boost.
The Fulmar I using 100 octane fuel was no faster once 10,000ft was reached which would probably be the case for a Sea Hurricane using a Merlin VIII engine.
To me there are two points at which a Sea Hurricane with folding could have been introduced or introduced earlier. The late 39/early 40 point where it replaces the Fulmar.
And the 2nd point in the Spring of 1941, The Hurricane II with Merlin XX engine had been in production for over 6 month, The Spitfire was the choice of the RAF, they just needed more of them.
The FAA did not get a Sea Hurricane II with Merlin XX for another full year. Spring of 1942 was when they started work converting the first Hurricane IIs.
The lack of a folding wing Hurricane in late 1939 maybe quite understandable. Waiting until May of 1942 to make fixed wing Hurricane IIS takes a lot of explaining.
What puzzles me is why the engine was only using 4lbs of boost using 87 octane fuel. The Merlin III with a higher supercharger gear (and higher temperature in the intake charge used 6lbs.The 4lb boost was testing done using 87 Octane fuel, and that accounts for the increase in speed at 9lb boost. The FTH of the Merlin VIII was only 2400ft at 9lb boost:
Merlin VIII 87 octane TO power was 5.75lb boost at 3000rpm but boost levels fell above SL. I guess 4lb boost was used because it could be held until 7000ft in climb and 9000ft in level flight.What puzzles me is why the engine was only using 4lbs of boost using 87 octane fuel. The Merlin III with a higher supercharger gear (and higher temperature in the intake charge used 6lbs.
The Merlin X in the Whitley used 5 3/4s for both take-off and and the 5 minute limit.
In fact the Merlin X in the Whitley was allowed 5 3/4s at 2600rpm for 1/2 hr climb rating.
4lbs was the max rich cruise limit.
Whitley manual gives higher limits for 100 octane but 4lbs seems low even for 87 octane for the Fulmar I.
I am still having trouble with it.Merlin VIII 87 octane TO power was 5.75lb boost at 3000rpm but boost levels fell above SL. I guess 4lb boost was used because it could be held until 7000ft in climb and 9000ft in level flight.
The Merlin X used a two speed SC and would switch to FS gear almost immediately after TO. Similarly the 87 Octane version Merlin X MS gear and rotor was chosen for max power at SL to get heavily laden bombers off the airfield and then they would switch to FS gear.
According to Fulmar Pilot's Notes Merlin VIII 87 octane TO was 3000rpm/5.75lb and the 5min limit was 3000rpm/4lb.I am still having trouble with it.
If the supercharger would only give 5.75lbs boost at sea level with 87 octane it would only give 5.75lbs with 100 octane.
There had to be some point were it was giving 5.75 with a wide open throttle and I am guessing some were around 5-6000ft.
Best rate of climb was at 7000ft which would indicate that was where the FTH was + whatever RAM effect they had from the climbing speed.
FTH in level flight was at 9,000ft as you say.
Merlin VIII used as 6.313 supercharger gear and the Merlin X used a 6.389 supercharger gear. 1.2% different.
we know that the Merlin X would give 1130hp at 5250ft in low gear from the Halifax data sheet. Or 1145hp at 5250ft from the 1938 Janes which is close enough, not going to argue about 15hp on an 1100hp engine from sources 3 years apart.
They were using 3.5lbs of boost in Kestrels with 87 octane fuel (and higher for take-off) . They were using 6lbs of boost in the Merlin C.
I am not saying the test wasn't done at 4lbs, but we don't know why.
Which in hindsight seems extraordinarily silly. The Soviets didn't really want the Hurricanes anywayEven supplying Hurricane II to the USSR was rated a higher priority than supplying the FAA in late 1941 / early 1942. Any attempt to have given the Soviets such poor quality Hurricane I would have seen them rejected at the dockside.
You just needed to get the 100 octane fuel to your carrier. Not really a problem in the summer of 1940 and later. Might make difference on what you planning to buy in 1939 and build in 1940. The 100 octane supply turned out to be not as big a deal as they thought but that is hind sight.Just one observation regarding the use of 100 Octane fuel. It was the standard fuel in RAF fighters around May 1940 and use had been approved in Sept 1939. The changes needed to convert an aircraft to use 100 Octane from 87 octane were minimal and you didn't need to make any plan to purchase new aircraft.
The Perseus used 9 Hercules cylinders instead of 14 for good and for ill.British mechanics were all ready used to working on bizarre British stuff, one more wouldn't kill them
And yet they accepted around 3,000 of them from British and Canadian production lines between 1941 & 1944. By Sept 1942 some 15 regiments had been trained to use them. On 1 May 1945 some 750 remained in the Red Army Air Force inventory, mostly with the Air Defence Force.Which in hindsight seems extraordinarily silly. The Soviets didn't really want the Hurricanes anyway