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Figure 9 shows a free body diagram for an aeroplane flying at a constant speed and at a constant height - AQA - GCSE Physics Combined Science - Question 6 - 2019 - Paper 2

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Figure 9 shows a free body diagram for an aeroplane flying at a constant speed and at a constant height. The speed of the aeroplane is much greater than the speed a... show full transcript

Worked Solution & Example Answer:Figure 9 shows a free body diagram for an aeroplane flying at a constant speed and at a constant height - AQA - GCSE Physics Combined Science - Question 6 - 2019 - Paper 2

Step 1

Explain how the forces need to change so the aeroplane can land.

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Answer

To allow the aeroplane to land safely, the forces acting on it must adjust as follows:

  1. Decrease in Thrust: The thrust must decrease as the aeroplane prepares for landing. This allows for proper slowing down and helps control the descent.

  2. Increase in Air Resistance: As speed decreases, air resistance or drag increases, opposing the thrust and contributing to the reduction in speed.

  3. Reduction in Lift: The lift force must also decrease. As the weight of the aeroplane remains constant, and if lift is less than weight, the aeroplane will descend.

  4. Introduction of Downward Force: Consequently, with a decrease in lift and sustained weight, there emerges a resultant downward force which assists in the controlled landing.

Step 2

Calculate the mass of the aeroplane.

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Answer

To calculate the mass of the aeroplane, we can use the equation of motion:

  1. Determine Deceleration:

    Using the formula for acceleration, we have: a=vfvit=10m/s80m/s28s=7028=2.5m/s2a = \frac{{v_f - v_i}}{{t}} = \frac{{10 \, m/s - 80 \, m/s}}{{28 \, s}} = \frac{{-70}}{{28}} = -2.5 \, m/s^2

  2. Calculate Resultant Force:

    We know that the mean resultant force ( F ) is given by:

    F=maF = m \cdot a

    Given that ( F = -750000 , N ) and ( a = -2.5 , m/s^2 $$, we can rearrange the formula to find mass ( m ):

    ( -750000 = m \cdot -2.5 )

    1. Solve for Mass:

    ( m = \frac{{-750000}}{{-2.5}} = 300000 , kg $$.

The mass of the aeroplane is therefore ( 300000 , kg ).

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