Youtube hearted comments of Keit Hammleter (@keithammleter3824).

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  10. 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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  20. 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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