• Part A The equation P U.(dm/dt) for the thrust on a rocket, can also be applied to an airplane propeller. In fact, there are two contributions to the thrust one posisve and one negative. T positive contribution comes from air pushed backward, away from the propeller (so drm/dt <0) at a speed tler relative to the propeller. The negative contribution comes from this same quantity of air fowing into the front of the propeller (so dm/dt > 0) at speed v. equal to the speed of the airplane through the air. For a Cessna 182 (a single-engine airplane) fying at 130 km/h, 150 kg of air flows through the propeller each second and the propeller develops a net thrust of 1300 N. Determine the speed increase (in km/h) that the propeller imparts to the air km/h

College Physics
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Chapter1: Units, Trigonometry. And Vectors
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Part A
The equation F
propeller. In fact, there are two contributions to the thrust one positive and one negative. The
positive contribution comes from air pushed backward, away from the propeller (so dm/dt < 0),
at a speed ver relative to the propeller. The negative contribution comes from this same quantity
Vez(dm/dt) for the thrust on a rocket, can also be applied to an airplane
For a Cessna 182 (a single-engine airplane) flying at 130 km/h, 150 kg of air flows through the propeller each second and the propeller develops a net thrust of 1300 N. Determine the speed increase (in km/h) that the propeller imparts
to t
of air flowing into the front of the propeller (so dm/dt > 0) at speed V, equal to the speed of the
airplane through the air.
km/h
Transcribed Image Text:Part A The equation F propeller. In fact, there are two contributions to the thrust one positive and one negative. The positive contribution comes from air pushed backward, away from the propeller (so dm/dt < 0), at a speed ver relative to the propeller. The negative contribution comes from this same quantity Vez(dm/dt) for the thrust on a rocket, can also be applied to an airplane For a Cessna 182 (a single-engine airplane) flying at 130 km/h, 150 kg of air flows through the propeller each second and the propeller develops a net thrust of 1300 N. Determine the speed increase (in km/h) that the propeller imparts to t of air flowing into the front of the propeller (so dm/dt > 0) at speed V, equal to the speed of the airplane through the air. km/h
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