![]() |
#341
|
||||
|
||||
![]() Quote:
__________________
|
#342
|
|||
|
|||
![]()
The 12lb boost calculation done by the RAE is an absolutely reasonable extrapolation.
|
#343
|
|||
|
|||
![]()
I have my doubts about it having been made by RAE. It's an obvious farce.
__________________
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 ![]() |
#344
|
||||
|
||||
![]() Quote:
Well, then walk us through the explaination of how the engine data aligns with the graph. I would love to hear it. Performance graph showing FTH of 11,000 ft: http://www.spitfireperformance.com/s...-rae-12lbs.jpg Engine data with RAM effect at max level speed showing FTH of 8,500 feet: http://www.spitfireperformance.com/merlin3curve.jpg
__________________
|
#345
|
|||
|
|||
![]() Quote:
FTH at 17,000 ft (http://www.spitfireperformance.com/merlin3curve.jpg) Max level speed at 19,000 ft (http://www.spitfireperformance.com/s...-rae-12lbs.jpg) Looks like max level speed is achieved 2,000 feet above the FTH. Pretty much in line with the difference for +12 boost. Edit: I want to make clear that this 2,000 ft difference between FTH and max speed must not be present in reality, it's more a systematical difference between the two charts that must be considered when they are compared. Last edited by 41Sqn_Banks; 09-25-2012 at 01:05 PM. |
#346
|
||||
|
||||
![]()
That chart was not used because it does not align. The engine chart you linked already includes RAM effect at Vmax.
That means the FTH should match. Not be close or have the same margin of error, but match if that is the correct engine data. I used the power figures as listed in the flight reports NOT a seperate engine curve that does not match the performance data.
__________________
|
#347
|
||||
|
||||
![]()
__________________
|
#348
|
|||
|
|||
![]()
I know that, I can read. You asked how the engine data align with the speed graph. They align with an consistent altitude difference of about of 2,000 ft.
The altitude difference between the FTH in the charts can be explained by a different level flight speed. E.g. Hurricane I has a FTH of 17,750 ft at 316 mph. Spitfire I has a FTH of 18,600 ft at 364 mph. As we see the 50 mph speed difference results in a drop of 1000 ft for the FTH. There is nothing contradicting in the charts ... |
#349
|
||||
|
||||
![]() Quote:
Quote:
A speed difference is not going to account for a 2000 ft increase in FTH. How do you explain the fact this chart comes from an investigation of performance with an experimental high altitude engine. The chart exactly matches the one found in: Messerschmitt Me. 109 Handling and Manoeuvrability Tests BY M. B. MORGAN, M.A. and D. E. MORRIS, B.SC. COMMUNICATED BY THE PRINCIPAL DIRECTOR OF SCIENTIFIC RESEARC (AIR) MINISTRY OF SUPPLY __________________________________ Reports and Memoranda No. 2361 September 1940* http://kurfurst.org/Tactical_trials/...ls/Morgan.html
__________________
|
#350
|
||||
|
||||
![]() Quote:
AFAIK, the Spitfire Mk I was equipped with the Merlin III engine.
__________________
|
![]() |
Thread Tools | |
Display Modes | |
|
|