Home
Class 11
PHYSICS
A plane is in level flight at constant s...

A plane is in level flight at constant speed and each of its two wings has an area of `25 m^(2)` . If the speed of the air on the upper and lower surfaces of the wing are `270 km h^(-1)` and '234 km h^(-1)' respectively, then the mass of the plane is (Take the density of the air `=1 kg m^(-3)`)

A

1550 kg

B

1750 kg

C

3500 kg

D

3200 kg

Text Solution

AI Generated Solution

The correct Answer is:
To solve the problem step by step, we will follow these calculations: ### Step 1: Convert the speeds from km/h to m/s We are given the speeds of the air on the upper and lower surfaces of the wing: - Speed on the upper surface (V2) = 270 km/h - Speed on the lower surface (V1) = 234 km/h To convert these speeds to meters per second (m/s), we use the conversion factor \( \frac{5}{18} \): \[ V1 = 234 \times \frac{5}{18} = 65 \, \text{m/s} \] \[ V2 = 270 \times \frac{5}{18} = 75 \, \text{m/s} \] ### Step 2: Calculate the pressure difference using Bernoulli's principle According to Bernoulli's principle, the pressure difference between the upper and lower surfaces of the wing can be expressed as: \[ P1 - P2 = \frac{1}{2} \rho (V2^2 - V1^2) \] Where: - \( \rho \) = density of air = 1 kg/m³ Substituting the values: \[ P1 - P2 = \frac{1}{2} \times 1 \times (75^2 - 65^2) \] Calculating \( 75^2 \) and \( 65^2 \): \[ 75^2 = 5625, \quad 65^2 = 4225 \] Thus, \[ P1 - P2 = \frac{1}{2} \times 1 \times (5625 - 4225) = \frac{1}{2} \times 1 \times 1200 = 600 \, \text{N/m}^2 \] ### Step 3: Calculate the total upward force on the wings The total upward force (F) acting on the wings can be calculated using the pressure difference and the area of the wings: \[ F = (P1 - P2) \times A \] Where: - \( A \) = total area of the wings = \( 25 \, \text{m}^2 \times 2 = 50 \, \text{m}^2 \) Substituting the values: \[ F = 600 \, \text{N/m}^2 \times 50 \, \text{m}^2 = 30000 \, \text{N} \] ### Step 4: Relate the upward force to the weight of the plane In level flight, the upward force equals the weight of the plane (mg): \[ mg = 30000 \, \text{N} \] ### Step 5: Calculate the mass of the plane To find the mass (m) of the plane, we use the acceleration due to gravity (g = 10 m/s²): \[ m = \frac{F}{g} = \frac{30000 \, \text{N}}{10 \, \text{m/s}^2} = 3000 \, \text{kg} \] ### Final Answer The mass of the plane is \( 3000 \, \text{kg} \). ---

To solve the problem step by step, we will follow these calculations: ### Step 1: Convert the speeds from km/h to m/s We are given the speeds of the air on the upper and lower surfaces of the wing: - Speed on the upper surface (V2) = 270 km/h - Speed on the lower surface (V1) = 234 km/h To convert these speeds to meters per second (m/s), we use the conversion factor \( \frac{5}{18} \): ...
Promotional Banner

Topper's Solved these Questions

  • MECHANICAL PROPERTIES OF FLUIDS

    NCERT FINGERTIPS ENGLISH|Exercise Higher Order Thinking Skills|8 Videos
  • MECHANICAL PROPERTIES OF FLUIDS

    NCERT FINGERTIPS ENGLISH|Exercise Exemplar Problems|5 Videos
  • LAWS OF MOTION

    NCERT FINGERTIPS ENGLISH|Exercise Assertion And Reason|15 Videos
  • MECHANICAL PROPERTIES OF SOLIDS

    NCERT FINGERTIPS ENGLISH|Exercise Assertion And Reason|15 Videos

Similar Questions

Explore conceptually related problems

A plane is in level flight at constant speed and each of its wings has an area of 25m^(2) . If the speed of the air is 180km//h over the upper wing surface, determine the plane's mass . (Take air density to be 1 kg//m^(3) ). g=9.8m//s^(2) .

In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are 70 ms^(-1) and 63 ms^(-1) respectively. What is the lift on the wing if its area is 2.5 m^(2) ? Take the density of air to be 1.3 kg m^(-3)

In a test experiment on a model aeroplane in a wind tunnel, the flow speeds on the upper and lower surfaces of the wing are 70ms^(-1) and 83ms^(-1) respectively. What is the lift on the wing, if its area is 2.5m^(2) ? Take the density of air to be 1.3kgm^(-3)

The speed of flow past the lower surface of a wing of an aeroplane is 50ms^(-1) . What speed of flow over the upper surface will give a dynamic lift of 1000 pa ? Density of air =1.3 kgm^(-3)

A fully loaded Boeing aircraft has a mass of 3.3xx10^(5) kg . Its total wing area is 500 m^(2) . It is in level flight with a speed of 960 km//h . (a) Estimate the pressure difference between the lower and upper surfaces of the wings (b) Estimate the fractional increases in the speed of the air on the upper surfaces of the wing relative to the lower surface. The density of air is 1.2 kg//m^(3) .

Air stream flows horizontally past an aeroplane wing of surface area 4 m^(2) . The speed of air over the top surface is 60 ms^(-1) and under the bottom surface is 40 ms^(-1) The force of lift on the wing is (density of air = 1 kgm^(-3) )

An aircraft of mass 4 xx 10^(5)kg with total wing area 500m^(2) in level flight at a speed of 720 km h^(-1) . The density of a at its height is 1.2 kgm^(-3) . The fractional increases in the speed of the air on the upper surface of its wings relative to the lower surface is (take g = 10 ms^(-2) )

An aeroplane of mass 3xx10^(4)kg and total wing area of 120 m^(2) is in a level flight at some height the difference in pressure between the upper and lower surfaces of its wings in kilo pascal is (g=10m//s^(2))

The speed of a car is 72 km h^(-1) . Express it in m s^(1)

Air is streaming past a horizontal airplane wing such that its speed is 90 ms^(-1) at the lower surface and 120 ms^(-1) over the upper surface. if the wing is 10 m long and has an average width of 2 m , the difference of pressure on the two sides and the gross lift on the wing respectively, are (density of air =1.3kgm^(-3) )