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In article ,
"xerj" wrote: Thrust from a propeller drops as speed increases to a theoretical zero. When this happens, what is providing the thrust to overcome drag? The forward momentum of the aircraft? If so, is it a case of the speed very slightly and imperceptibly dipping below the zero thrust speed, getting a little thrust to bring it back to the zero-thrust condition and doing this over and over again? Thanks in advance. On a reciprocating engine, you have only so much power available. In level flight: Power = Thrust * Velocity. Or: Thrust = Power/Velocity. If you go faster, thrust decreases to meet power. Thrust, theoretically, will not go to zero, but will equal drag, which increases with the square of velocity. If you dive, thrust is added by the weight of the aircraft * sine of the dive angle. -- Remve "_" from email to reply to me personally. |
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![]() xerj wrote: If so, is it a case of the speed very slightly and imperceptibly dipping below the zero thrust speed, getting a little thrust to bring it back to the zero-thrust condition and doing this over and over again? Nope, all things being maintained constant, the aircraft maintains a steady state equilibrium. Dave |
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