Originally posted by Robert
Manifold pressure resumes. La7 has the same Manifold pressure
drop at the same alts. Then regains the same pressure at 17k
just like a 2 stage charger. If it doesnt have the 2 stage charger
shouldnt it's Manifold pressure continue to drop as you gain
more alt.
RWY
.
Your observations are correct and the AH indicated manifold pressure curve of the La7 and La5 are incorrect IMO at mid altitudes.
Height______Boost______Speed (IAS)
M_________mm.pt.ct_______ Km/h
0000________1000________ 270
1000________1000_________270
2000________1000_________270
3000_________900_________265
4000_________825/1000____260 (2nd stage/speed of boost)
5000________1000_________255
6000_________900_________250
7000_________765_________240
8000_________660_________240
9000_________600_________235
10000________550_________230
These figures are off an August 44 La7 climb rate test and show only the non WEP (2400rpm) boost v altitude.
WEP (2500 rpm) generates 1180mm (46.46") of boost upto approx 2000m+ (6600ft) where it fades to 1000mm (39.37") by about 2600m (8500ft)
You will also note that this is at max climb so there is little RAM air effect at the intake.
In AH units this would read
Height______Boost______Speed (IAS)
Ft__________inches________m/h
0000________39.37_________168
3278________39.37_________168
6557________39.37_________168
9836________35.43_________165
13114_______32.48/39.37____161 (2nd stage/speed of boost)
16393_______39.37_________158
19672_______35.43_________155
22950_______30.11_________149
26230_______25.98_________149
29508_______23.62_________146
32786_______21.65_________143
Manifold pressures indicated and given in the E6b are therefore slightly erronious IMO (for both La5Fn and La7).
WEP boost was 46.5" not 48". Mil power was 39.4" not 41".
The 2nd stage of boost is permitted at just over 13K and not at 16>17K as the Lavochkin cockpit manifold gauges indicates.
In fact if you refer to AH's own climb rate curve for the La5FN & La7 you will see that the 2nd SC speed step is about 13K and maintained as per the above test until 16.5>17K.

The various speeds and climb rates modelled seem to be pretty much spot on for a fully tested production model however. So we may be being fussy and the only performance curve affected due to any error may be limited to fuel consumption rates at the differring altitudes.