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Btw, about the P-51's Clmax figure, this is lower according to NACA which lists it as 1.35.
I admit 1.47 is my own estimate..
Ofcourse HP means nothing without knowing prop efficiency, but the speeds of the a/c compared to the overall drag give a very good idea of this.
As for weights, well it has already been chosen = Full weight for all a/c except the -51 which is left with empty fuselage tank. The reason for this is I understand that P-51 pilots on escort missions would rely on fuel from the fuselage tanks first to empty it, and then swith over to the external tanks until they had to be dropped. This way the CG stayed within the right range.
None of those saw service though..
On 18 September 1944 ADGB noted, that with respect to the Mustang III/Packard Merlin 1650-7, "A total of over 7,000 hours have been flown at a maximum boost pressure of + 25 lbs./sq. in.". 25 The RAF's Mustang Pilot's Notes gives the Combat Engine Limitation as "81 ins. boost for 5 minutes when using 150 grade fuel". 26 Combat Reports show +25 lbs was used operationally over the continent by UK based Mustangs of ADBG
Those are no P-51D's ponsford, those are Mustang Mk.III's.
The Mustang III's boosted that much were used for V1 hunting IIRC and did not encounter any enemy fighters. And as for P-51D's, well AFAIK only one was tested running at +25 lbs/sq.in. boost, and with a RR engine.
That doesn't change the fact that the RAF had operational Mustangs employing +25 lbs boost with BHP of 1940 BHP.
Bada,
Thanks but I already have it.
Bill,
We can also do it with full fuselage tank but that would be abit unfair I think seeing that the pilots were adviced to empty this first so as to correct the CG. We can also simulate the 40% reduction of fuel load at the time period you mention.
By comparison it wasn't uncommon for German fighters to take off with half fuel tanks, fuel being in desperate demand.