![]() |
|
FM/DM threads Everything about FM/DM in CoD |
![]() |
|
Thread Tools | Display Modes |
|
#1
|
|||
|
|||
![]()
I'm sorry lane, I got that part wrong, I stand corrected. The Merlin Mk XX was used introduced in August, first it was fitted to modified Mk Is made to Mk II standard at the factory, then on the Hurricane Mk II which was introduced to squadron service in September 1940. So it was indeed present in the BoB.
Regardless the salient point still stands in that CoD does not have a flyable aircraft with a Merlin XX. I think it is worth mentioning that the Merlin XII of the Spitfire Mk II introduced a 70/30% water/glycol coolant mix. This new mix improved cooling abilites and was safer than the 100% glycol mix of the earlier Merlin Variants as used in the Mk Ia. Having said that, it was not a magic mixture that = no more overheat. I agree with Seadog that we need +12lbs boost for the RAF fighters, but I dont agree it could be used all day long without potential consequences. Incidentally the Spitfire Mk IIa is already running at +12lbs boost speeds. Last edited by ICDP; 06-06-2011 at 06:02 PM. |
#2
|
|||
|
|||
![]()
Historically, if you were in a Merlin III powered fighter and you needed to use 12lb boost, you did so, and you damned the consequences because staying alive and/or destroying the enemy was more important than explaining away a broken engine. 12lb boost/3000rpm will not cause overheating in level flight. It might cause overheating in prolonged max angle of attack climbs as per Dowding's memo of Aug 1, 1940 but other combat manoeuvres were probably the prime culprit in causing increased engine wear leading to bearing failure, also as per Dowding's memo.
|
#3
|
|||
|
|||
![]() Quote:
|
#4
|
|||
|
|||
![]() Quote:
http://www.wwiiaircraftperformance.o...bs-14nov39.jpg Basically, it is a question of modelling the cooling and lubrication capability of the aircraft and in straight and level flight 12lb/3000rpm will not cause problems but pilots need to keep a watch on their oil pressure, temp and engine coolant gauges during prolonged steep climbs, and their engine RPM during dives. So if I am chasing/being chased by a 109 and I'm in level flight and I pull the boost override, I have a very high probability of being able to run at 12lb/3000rpm until I run out of fuel. If I make repeated steep climbs and let my temps and pressures stay in the red, then my probability of engine failure increases. It is a question of accurate flight modelling. |
#5
|
|||
|
|||
![]() Quote:
|
#6
|
|||
|
|||
![]()
I should have been clearer from the start in stating that straight and level and/or turning flight was unlikely to be problematic at 12lb/3000rpm because the cooling and lubrication system could cope with it (gauges stay within normal parameters). I suspect that there might be differences between the various aircraft in steep climbs and 12lb/3000rpm in terms of cooling capability but accurate flight modelling will provide danger warnings to the pilot as his gauges go into the red.
Last edited by Seadog; 06-06-2011 at 08:01 PM. |
#7
|
||||
|
||||
![]()
The Merlin was cleared for +12lb on Take off and that could be used for "short duration" in an emergency. It was so limited, that it was not cleared for even ONE full minute much less FIVE.
It clearly states that the engine is highly overloaded when using +12lb boost. Furthermore, using it for short duration outside of take off, immediately deadlines the engine until it is inspected by a mechanic and cleared for re-entry into service. How do those very clear instructions get translated into "could use +12lbs continuously"? ![]() The endurance testing quoted in this thread is extremely limited for an endurance test. Most engines are ran continuously for far longer time periods at the emergency conditions during endurance trails with resulting tolerance wear. The Merlin was run for only 5 minutes at a time with a 20 minute rest period between. In that context, the Merlin endurance trials at +12lbs were not successful and the results are far from the "idea" that the Merlin was cleared to run +12lb continuously. Last edited by Crumpp; 06-07-2011 at 06:00 PM. |
#8
|
|||
|
|||
![]()
I am curious on what do you base the above, especially as the engine's coolant system was designed for some 30% lower engine outputs..
__________________
Il-2Bugtracker: Feature #200: Missing 100 octane subtypes of Bf 109E and Bf 110C http://www.il2bugtracker.com/issues/200 Il-2Bugtracker: Bug #415: Spitfire Mk I, Ia, and Mk II: Stability and Control http://www.il2bugtracker.com/issues/415 Kurfürst - Your resource site on Bf 109 performance! http://kurfurst.org ![]() |
#9
|
|||
|
|||
![]()
Because +12 in level flight = fast, and the cooling system was designed for the max climb case. Flying twice as fast doubles the mass flow rate through the radiator, and thus the heat rejection capability at constant radiator matrix temperature.
If you've got enough radiator for the climb case, you've almost always got too much for high speed level flight - hence the need for variable geometry. |
#10
|
|||
|
|||
![]()
Pity it doesn't work as such in CoD... I mean temp goes up like mad in a moment if you set the radiator flaps too narrow, almost regardless of aircraft speed. :/
__________________
Il-2Bugtracker: Feature #200: Missing 100 octane subtypes of Bf 109E and Bf 110C http://www.il2bugtracker.com/issues/200 Il-2Bugtracker: Bug #415: Spitfire Mk I, Ia, and Mk II: Stability and Control http://www.il2bugtracker.com/issues/415 Kurfürst - Your resource site on Bf 109 performance! http://kurfurst.org ![]() |
![]() |
|
|