Follow along with the video below to see how to install our site as a web app on your home screen.
Note: This feature may not be available in some browsers.
Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
One vs one, LW fighters have a substantial lead in performance historically. In 1940, the 109E (350 mph) is ahead of early Zero (320-330 mph), the 109F1/F2 is at ~620 km/h (plus 10-15 km/h when over-revving the DB 601N at 2800 rpm), with 109F4 to extend this performance over 30 minutes vs. 3 min only with 109F1/F2.
The Fw-190, assumed it is ready to be deployed and used that much away from tidy bases, will bring another performance boost vs. the Japanese, something like what Marine Corsairs and USAF Lightnings were providing, but without the legs and without P-38-intristic problems; ditto the Bf-109G2 and fully rated Bf-109F4.
What about airfields? How many airfields would have been able to accommodate large, long-range transport aircraft? The likes of converted Fw-200s and, slightly later, Ju 252s would be very useful, albeit more costly for fuel used and unlikely practical to supplant land/sea supply routes. (perhaps enough to fill the gaps for whatever materials/resources/personnel were least possible to move on the ground or at sea)
That said, managing supply routes through British/French (possibly some Dutch) held territories might be more practical, especially if they weren't sending equipped troops, but unequipped personnel with military equipment being sold to China separately and the supplemental forces being equipped once they reached Chinese soil.
Historically Stalin allowed millions of tons of trade between Germany and Japan via the USSR's railroads from 1940-41:And saying that Stalin would just let a massive army and supply-line snake across his country is ridiculous. Not only is Stalin dangerously paranoid, but that is asking a tremendous amount of trust on behalf of Hitler, who was dellusional beyond beleif. Also, how well would Germany be able to move this tremendous amount of equipment all the way over to China during winter and spring? They couldn't even move equipment on the road to Stalingrad.
In September 1937, the Soviet leadership signed the Sino-Soviet Non-Aggression Pact and approved Operation Zet, the formation of a Soviet volunteer air force. As part of this secret operation, Soviet technicians upgraded and ran some of China's transportation systems. Bombers, fighters, supplies and advisors arrived, including Soviet general Vasily Chuikov, the future victor of the Battle of Stalingrad. Prior to the entrance of the Western Allies, the Russians provided the largest amount of foreign aid to China, totalling some $250 million in credits for munitions and other supplies. In April 1941, Soviet aid ended as a result of the Soviet–Japanese Neutrality Pact and the beginning of the Great Patriotic War.
This is very significant and may clear up some of the range discrepancies for the Bf 110 figures as well.
It seems range at economical cruise with drop tank wasn't much worse than the P-40C or P-39D, and possibly better than the Spitfire Mk.II.
Any time figures look too good to be true, they probably are. The P-40 was heavy and couldn't climb worth rotten apples ( using normal power, ie non WEP) but it had a rather similar drag to the 109E ( about the same speed for about the same power) so cruise power should be about the same. P-40 carried about 40% more internal fuel than a 109, once you figure in warm up, take off and reserves it is hard to believe that the 109 can go as far on that much less fuel.
A P-40 clean running 375kph at 12,000ft (3636 meters?) was burning one gallon for every 5.5 miles traveled or about 0.43 liters per km, just about the same as a 109E. Even if this figure is off by 10% it doesn't make up for the 40% more fuel in the P-40.
Granted the US drop tank is smaller so with external tanks things equalize somewhat.
Revised versions of the P-40 soon followed: the P-40B or Tomahawk IIA had extra .30 in (7.62 mm) U.S., or .303 in (7.7 mm) machine guns in the wings and a partially protected fuel system; the P-40C or Tomahawk IIB added underbelly drop tank and bomb shackles, self-sealing fuel tanks and other minor revisions, but the extra weight did have a negative impact on aircraft performance. (All versions of the P-40 had a relatively low power-to-weight ratio compared to contemporary fighters.)
This seems to be at odds with at least one book showing range/fuel consumption charts ( or facsimile) for a 109E. Using a cruise setting of 2200-2400rpm and 1.15 ATA and speeds are about 455/520kph at 3000/5000meters and fuel used in 0.64/0.63 liters per km. or just under 400 miles not inclusive of take-off,climb and reserves. Using 1400/1600rpm and 0.76/0.63 ata at 3000/5000 meters gives speeds of 350/360kph and a fuel burn of 0.43 liters per km at both altitudes. range is now 576 miles not inclusive of take-off,climb and reserves
I thought the P-40B was actually pretty hampered by its modifications:
Curtiss P-40 Warhawk - Wikipedia, the free encyclopedia
Sorry, see here for P-40E:
http://zenoswarbirdvideos.com/Images/P-40/P-40FOIC.pdf
The earlier versions might actually do a bit better fuel consumption wise. Point is that 600 miles plus for a 109E without drop tank is pretty much a fantasy.
The 109F is somewhat better.
...
This seems to be at odds with at least one book showing range/fuel consumption charts ( or facsimile) for a 109E. Using a cruise setting of 2200-2400rpm and 1.15 ATA and speeds are about 455/520kph at 3000/5000meters and fuel used in 0.64/0.63 liters per km. or just under 400 miles not inclusive of take-off,climb and reserves. Using 1400/1600rpm and 0.76/0.63 ata at 3000/5000 meters gives speeds of 350/360kph and a fuel burn of 0.43 liters per km at both altitudes. range is now 576 miles not inclusive of take-off,climb and reserves
... The Fw 190 had room for fuel in the wings where the outer gun stations were though I know that this was to be used only on the Fw 190D13 (which had deleted the outer guns and compensated with a motor gun). The Me 109G with a 1320hp engine was faster than a P-40F or N with a more powerful engine.
The Me 109 wings seem to have been full of the pilots liquid oxygen supply though there must have been some room as I believe the Nitrous Oxide might be carried there as well.
I believe the Bf 109E actually had more fuel than the Me 109F
Why is the E having that range fantasy given the post by Koopernic? Also your charts for the D&E, not the B that the Flying Tigers flew.
Do you have power versus altitude charts for the DB601 vs Allison?
...
This seems to be at odds with at least one book showing range/fuel consumption charts ( or facsimile) for a 109E. Using a cruise setting of 2200-2400rpm and 1.15 ATA and speeds are about 455/520kph at 3000/5000meters and fuel used in 0.64/0.63 liters per km. or just under 400 miles not inclusive of take-off,climb and reserves. Using 1400/1600rpm and 0.76/0.63 ata at 3000/5000 meters gives speeds of 350/360kph and a fuel burn of 0.43 liters per km at both altitudes. range is now 576 miles not inclusive of take-off,climb and reserves
...
Range of an Me 109E4 was about 410 miles at maximum cruise inclusive of climb and reserves. Slow the aircraft to economical cruise and the range goes up to around 1100km (650 miles). Add a 300L drop tank to supplement the 400L internal fuel the ranges are about 650 miles and 1000 miles respectively.
Me 109's also seem to be able to cruise at speeds almost as fast as Japanese maximum speeds: this is what was essential in the European context. The Me 109 like the Spitfire was designed to intercept an enemy aircraft that might have risen from an airfield only a few dozen kilometres away.
Note, I believe the DB601Aa (a for ausland (foreign export) had a different supercharger ratio setup that gave a lower FTH) they were used on Luftwaffe aircraft nevertheless.
...
I believe the Bf 109E actually had more fuel than the Me 109F
The range table for the Bf-109E: link.
At 5 km, it is supposed to do 460 km (286 miles) on max continuous power (1.15 ata, 2400 rpm) while making 520 km/h TAS (440 km/h IAS), or 665 km (413 miles) on 'max range' setting (0.76 ata, 1400 rpm) while making 350 km/h TAS (270 km/h IAS). Of course, those figures don't cover the fuel used for warm-up, climb, combat and reserves.
I doubt fuel injected engines need any warm up. I'm old enough to remember cars with chokes and the 30 seconds of fiddling with them, now I just drive off.