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#4
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This question was posed at our retired engrs coffee shop group this AM
where such weighty issues are discussed ad nauseum. The consensus was that probably minimum-engine prop dynamic structural stresses (stresses other that the engine output torque and engine output torque pulses - i. e. due to gryroscopically induced moments applied to the crankshaft) will occur if the prop is vertical at the point of maximum yaw velocity. How that translates into a rough running system given the engine mount system is not obvious. I didn't personally experience the roughness of the original 172M that had the improperly indexed prop, so I can't verify that the roughness was first order as I originally stated. I just assumed it was. At any rate, I still put my money on the prop orientation being optimized to the second harmonic yaw motion of the engine. The reaction and rebound of a individual cylinder firing moving the crankcase. I'm not sure but some of it maybe also be attributed to camshaft and valve spring pressure. Valve train forces are much higher than you might first suspect. The forces generated and reacted within the engine, stay within the engine. They don't reflect outside. The whole problem of roughness however, has to be considered with the possibility that the prop or engine has a first order out-of-balance that is dominating any observer's attention. |
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