Pressure and lift force on a wing

In summary, the airplane in question has a mass of 1.60-10^4 kg and each wing has an area of 40.0m^2. During level flight, the pressure on the lower wing surface is 7.00-10^4 Pa. To determine the lift force on the plane, the formula Force (N) = Pressure (N/m2) * Area (m2) can be used. For the plane to lift off, the net force on the wing must be upward and equal to the weight of the plane.
  • #1
physixnot4me
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An airplane has a mass of 1.60-10^4 kg and each wing has an area of 40.0m^2. During level flight, the pressure on the lower wing surface is 7.00-10^4 Pa. Determine the LIFT FORCE on the plane. Is it sufficient to lift the plane?

part is what concerns me: if it is in level flight, the net force is zero

How do I go about answering this question... leading me in the right direction would be very helpful =) Big thanks!
 
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  • #2
Force (N) = Pressure (N/m2) * Area (m2)

and the upward force must equal the weight of the plane.

For a plane to 'fly' the pressure above the wing must be lower than the pressure below the wing, so that the net force on the wing is upward and equal to the weight of the plane.
 
  • #3


I would approach this question by first understanding the principles of pressure and lift force on a wing. Pressure is a force per unit area and is exerted by a fluid, such as air, on any object that is in contact with it. In the case of an airplane wing, the shape and angle of the wing creates a difference in pressure between the upper and lower surfaces, resulting in a net upward force known as lift force.

To determine the lift force on the plane, we can use the following equation: Lift force = pressure x wing area. Plugging in the given values, we get: Lift force = (7.00-10^4 Pa) x (40.0m^2) = 2.80-10^6 N.

Now, the question asks whether this lift force is sufficient to lift the plane. As mentioned earlier, in level flight, the net force on the plane is zero. This means that the lift force is balanced by the weight of the plane, which is equal to its mass (1.60-10^4 kg) multiplied by the acceleration due to gravity (9.8 m/s^2). Therefore, the weight of the plane is 1.57-10^5 N.

Comparing the lift force (2.80-10^6 N) to the weight of the plane (1.57-10^5 N), we can see that the lift force is more than sufficient to lift the plane. This is because the lift force is greater than the weight of the plane, resulting in a net upward force that keeps the plane in level flight.

In conclusion, the lift force on the plane is 2.80-10^6 N and it is sufficient to lift the plane in level flight.
 

Related to Pressure and lift force on a wing

1. What is pressure and lift force on a wing?

Pressure and lift force on a wing are two important concepts in aerodynamics. Pressure is the force per unit area exerted by a fluid, such as air, on a surface. Lift force is the upward force that acts on an object when it is moving through a fluid, such as an airplane wing.

2. How is pressure and lift force related to the shape of a wing?

The shape of a wing plays a crucial role in determining the amount of pressure and lift force it experiences. A curved or cambered shape on the top surface of a wing creates a longer path for the air to travel, resulting in a lower pressure and higher velocity. This difference in pressure creates a lift force on the wing.

3. What factors affect the pressure and lift force on a wing?

The pressure and lift force on a wing are affected by various factors such as the shape of the wing, the angle of attack, the airspeed, and the density of the air. These factors can be manipulated to control the amount of lift force and ultimately, the flight of an aircraft.

4. How does an airfoil design contribute to pressure and lift force on a wing?

An airfoil is a specialized shape that is designed to create lift force when air flows over it. The curved shape on the top surface of an airfoil creates a lower pressure, while the flat bottom surface creates a higher pressure. This pressure difference creates a lift force on the wing, allowing an aircraft to fly.

5. How is lift force on a wing measured?

Lift force on a wing can be measured using various methods, such as wind tunnel testing, computational fluid dynamics, and flight testing. In wind tunnel testing, sensors are used to measure the forces acting on a model of the wing. In flight testing, sensors on the aircraft can provide data on the lift force experienced during flight. Computational fluid dynamics uses computer simulations to predict the lift force on a wing based on its design and operating conditions.

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