Originally posted by funkedup:
Dowding,
And I'm saying that the actual power of the engine in the aircraft is affected by the induction system, and the La-7 had a much better induction system than the La-5FN.
[ 09-20-2001: Message edited by: funkedup ]
Rated manifold presures for the Ash82FNV were the same in both the La5FN and the La7 (yes some late La5FN's had the V varient)
I belive the cowling design on the La 7 to have greatly aided cooling............
Exhaust arrangement aided aerodynamics more than any thing else....
Whilst the air intake was more aerodynamic it became a problem in the south during the last months of the war. It picked up dust that the over nose version did not. (not a problem during the wet autumn & winter of 44 / 45)
Vermillion and dowding hit the nail on the head generally...
Also I agree that the e retention seems too high ...particularly in engine off or idle mode and even more so in manouvering..rudder and elevator surface areas are massive inproportion to the rest of the AC.
Further in a sustained dive all 109 variants (well g4 onwards at least) should pull away after a few seconds.
However below 10K the La7 had more e than a 109 in the vertical (ie in a zoom climb)
This all means that although refined from the La5FN the La7 was still basically brute force and high wing loadings etc etc
If any one can show me an authentic la5FN performance curve with its WEP band I would like to see it! (I have them (with WEP) for the La7, La5 la5F but the La5FN never shows WEP) Further I have reports stating that the WEP period was limited to 2 mins from take off in the La 5FN.
Also the La7 top speed with WEP is generally shown to be faster (below 8k)than AH by a few MPH. (however IMHO it is more important that the AC is comparable to others than hitting some spec target smack on)
However I would state that the present departure point is at too high a speed by at least 20mph IAS (level)...... I do not believe the slats are properly modelled even if someone has tried to take them into account in the snap like departure characturistic. Reccommended landing speed was 135 km/hour with full flaps (83 mph)please try this in AH.... you fall out the sky first.
Further the flaps in the La7 were controlled by a hydraulic lever. You pushed it one way to lower them and another to close them. There was no auto retract.
The rear armoured glass was far more easy to see thru than AH would have us believe. The cross profiles were thinner, made of glass and had a single wire of re enforce ment. (like the wires in the IL2m3screen) The top brace was thinner and the bottom corner braces were below the seat and certainly not obstructing view out of the AC.
The Svak 20 had longer barrels than the Mk151/20 . (120 cm v 110 cm) Thru engine version used on yaks had even a longer barrel.
Tony's "rapid fire" seems to confirm this although the B20 seems about the same. The b20 and Shvak had shorter breaches than the 151/20.
The Shvak had greater rate of fire (800 v 700 rpm) (The La 7 Shvak could be unjammed from the cockpit)
In conclusion and added to to other data re round weight, size and explosive content (which Vermillion used to have on his web site) I would venture that the Shvak 20 (99r)had better range and lethality at target then the 151/20 (82)
The 3 gun B20 was so rare on the "front" that there is an argument for perking it (except it would be then unfairly perking the 2 gun shvak version)
Tilt