Youtube hearted comments of Keit Hammleter (@keithammleter3824).
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Exactly right, although Britain's prestige went down hill also because she wanted Dominions to keep buying British manufactured goods, and those goods by post-war standards were of poor quality and delivered late or never due to strikes.
Armaments supplied by Britain to Australian forces in North Africa were of poor quality. For instance, British-made tanks broke down far too much, and would loose their tracks on turns. When the Australians had run out of operable tanks, they got American tanks as replacements. In theory these tanks were inferior - they were lighter and had smaller guns. But Australian crews called the "honeys" because they only broke down if a German gun actually got a direct hit. They didn't loose their tracks in the tightest turns, so they could race in, get a few shots off and mess up a few enemy vehicles, then turn around and clear off quick before the enemy gets himself organised and fires back.
I used to know Australian aircrew who first flew British aircraft in the War and then changed to American aircraft. They all said the US planes were easier to fly, more reliable, and much easier to fix when they did go wrong. When a British fighter plane was delivered, in its crates, it took several skilled mechanics a couple of days to get it in flying condition. They could have a crated American fighter flying within an hour, using one trained mechanic assisted by a couple of untrained helpers.
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VisioRacer is quite right - inline engines have more of a problem with crankshaft torsional vibration. It wasn't a problem with the old American inline 8 car engines due to low compression design, and low power output.
In the 1930's America, a long engine bay on a car was a status symbol. Post-war, long engine bays were considered ugly, and women drivers found long cars hard to park. So engines had to be shorter - hence V8's, not I8's, post war.
An additional minor advantage of V-engines is lower friction. For any given cylinder swept volume, you would expect the power lost in friction would be directly proportional to the number of cylinders. However, for any given cylinder size and number of cylinders, the V-formation has less friction than the inline form due to the staggering of peak loads on each crank throw.
For a while. I worked as the engineer for a dealer selling large industrial diesel engines. Over a whole range of an engine series, the cylinder size is always the same. One series we sold gave about 50 kW per cylinder, so if you needed 200 kW, you got an inline 4, if you wanted 300 kW, you got an inline 6, if you needed 400 kW, you got a V8, and if you needed 600 kW, you got a V12. And if you needed 800 kW, you got a V16. The V8 got the same size starter motor as the I4. The V12 got the same size starter motor as the I6. Of course the V16 had two starter motors fitted, each the same size as the one fitted to the V8 and I4. This is not the full picture though - for example the I4 cranked a bit faster that the V8. But the friction loads were close enough to allow starter motor standardization.
The V engines needed only slightly larger starting batteries too. So, all up, a V8 is cheaper than an I8 for example.
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Gee, that design of battery charger goes back to the 1930's, except for the use of 1960's style stud rectifiers instead of selenium. Don't these guys know you can now buy potted silicon bridge rectifiers at much lower cost? It looks like they are cutting up regular passivated steel sheet to make the core laminations instead of using proper transformer-type silicon steel - as far as I know transformer steel is only supplied already punched into laminations, bonded into C-cores or toroids, or supplied in bulk in huge coils.
Using regular steel would be a lot cheaper, but the energy efficiency will be low, due to considerable hysteresis and low permitted flux density. Efficiency will be lowered more due to burrs left during their guillotining, which will short the laminations. Normally, laminations are punched first and then passivated, which ensures good inter-lamination insulation.
They are grouping the laminations instead of 1:1 interleaving, which is normally regarded as poor practice in the transformer industry, but given the above points, and that it is a high leakage reactance design (desirable in a simple battery charger) it may be a good thing.
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Sergei, contrary to your comment at the end, I found your video interesting, at least to me. I am an Australian, I grew up on my father 's farm. The farm next door was owned by a Ukrainian guy who was a refugee from World War 2. He could barely speak any English - hello, bye, yes, no, how are you was about his limit. His wife had to do the shopping so she spoke English quite a bit better. Him and his wife and kids spoke what I gather was mostly Russian amongst themselves, but since I spent a lot of time with his son and on their farm from a very young age, I picked up a few words - enough to converse with him on simple everyday subjects.
He made it very clear that he absolutely HATED Russians. So in the context of the war in Ukraine now I was wondering if inherited hatred was a factor in Ukraine's spirited and deterrmined defence. From your video made before the "Special Military Operation", I gather not - just a typical bit of racial/cultural prejudice existed in recent years.
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At 8:59 while talking about the amount of air going through vs the thrust produced, Warped Perception states "most of the energy comes from the fuel." That's sort of right, as the fuel notionally supplies chemical energy though combustion, but he doesn't say that, and in his context it is misleading and confusing.
Jet engines operate stochiomentrically - that is the mass of air consumed must just equal the amount required to completely combust the fuel and no more. For hydrocarbon fuels, the mass of air must be about 15 times the mass of the fuel consumed. (Only the oxygen is used chemically - air is about 80% nitrogen which passes through chemically unchanged. The actual oxygen mass is about 3 times the mass of the fuel.)
What produces the net thrust in a jet engine is that combustion raises the volume of air/fuel mix such that the burning gasses can push against a greater area of the forward inside engine surface than the combustion chamber air inlet area. The burning gas pressure in the combustion chamber must be approx equal or a bit less than the incoming air pressure to the chamber as otherwise burning gasses would come out the front. Thus forward thrust is produced as the exhaust orifice, always much larger than the air inlet orifice size, cannot offer much more than surrounding air pressure.
Jet engines are most easily understood properly by first considering a ram-jet engine, which has no moving parts. Intake air is compressed by the forward motion forcing the air through a funnel, so reducing the area and raising the pressure. Again, as with a turbojet, the forward part of combustion chamber surface area must be greater than the chamber hole for the incoming air, and is much greater than the exhaust orifice back pressure.
Understand all that and you will not only understand that the mass of air is more important than the mass of fuel (both supply the pressure, and there's much more air than fuel), you will also understand that the efficiency of a jet engine (ram or turbo) is proportional to the compression ratio.
In World War The British Air Ministry and the Royal Air Force famously took no notice of Frank Whittle and his jet engine, because his design and available materials permitted only a very low compression ratio, and thus they knew the fuel consumption would have to be horrendous without needing to test it. The jet became practical when others (eg at Rolls Royce) redesigned it to have a better compression ratio).
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