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Ch 09: Work and Kinetic Energy
Chapter 9, Problem 9

A 737-800 jet airliner has twin engines, each with 105 kN thrust. A 78,000 kg jet reaches a takeoff speed of 70 m/s in a distance of 1100 m. (b) What is the increase in thermal energy due to rolling friction and air drag?

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1
Calculate the total work done by the engines. Use the formula for work, which is the product of force and distance. The total force is the sum of the thrusts from both engines, and the distance is the takeoff distance.
Calculate the kinetic energy of the jet at takeoff speed using the formula for kinetic energy, KE = 0.5 \times m \times v^2, where m is the mass of the jet and v is the takeoff speed.
Determine the work done against friction and air drag. This can be found by subtracting the kinetic energy at takeoff from the total work done by the engines.
Understand that the increase in thermal energy due to rolling friction and air drag is equal to the work done against these forces, as energy conservation dictates that this energy is converted into thermal energy.
Summarize that the increase in thermal energy is the amount of energy dissipated due to non-conservative forces (friction and drag) during the takeoff.

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Key Concepts

Here are the essential concepts you must grasp in order to answer the question correctly.

Thrust and Drag Forces

Thrust is the force produced by the engines to propel the aircraft forward, while drag is the resistance force acting opposite to the direction of motion, caused by air friction. In this scenario, the total thrust from the engines must overcome both the drag and rolling friction for the jet to accelerate to takeoff speed.
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Work-Energy Principle

The work-energy principle states that the work done on an object is equal to the change in its kinetic energy. In this case, the work done by the thrust must account for the energy lost to friction and drag, which can be calculated to find the increase in thermal energy due to these forces during the takeoff.
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Kinetic Energy and Thermal Energy

Kinetic energy is the energy an object possesses due to its motion, calculated as 1/2 mv², where m is mass and v is velocity. During the takeoff, some of the energy provided by the engines is converted into thermal energy due to friction and drag, which can be quantified to understand the energy losses in the system.
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