I think the diagram shows that explicitly.Donna14 said:
Yes, can you try and apply it here?Donna14 said:
Forget that equation for lift force. I assume there are more parts to this problem, which you didn't show us. Some of the given information may be needed for those -- or may just be extra information.Donna14 said:
The Bernoulli principle states that as the speed of a fluid (such as air) increases, its pressure decreases. This principle applies to small aircraft because as the air flows over the wings, it increases in speed, creating a lower pressure area above the wing and a higher pressure area below the wing. This pressure difference creates lift, which allows the aircraft to fly.
The shape of an aircraft's wings, specifically the curvature and angle of the wing, affects how the Bernoulli principle is applied. A curved or cambered wing creates a longer path for the air to travel over the top surface, resulting in a lower pressure and more lift. The angle of the wing, also known as the angle of attack, affects the speed and direction of the air flowing over the wing, further influencing the application of the Bernoulli principle.
No, the Bernoulli principle is only one factor in the lift of flying objects. Other factors such as the angle of attack, air density, and weight also play a role in determining lift. Additionally, some flying objects, such as helicopters and rockets, use different principles to generate lift.
The Bernoulli principle is directly related to airspeed. As the airspeed of the aircraft increases, the pressure difference between the top and bottom of the wing also increases, resulting in more lift. However, there is a maximum airspeed at which the principle can be applied before the air becomes too turbulent and the wing stalls, causing a decrease in lift.
While the Bernoulli principle is an important factor in the lift of small aircraft, it is not the only principle at play. As mentioned before, other factors such as air density and weight also affect lift. Additionally, the Bernoulli principle is more applicable to steady, subsonic flight and may not accurately explain lift in supersonic or highly maneuverable aircraft. It is also important to note that the Bernoulli principle does not explain the lift of inverted flight, as the air is flowing over the bottom of the wing instead of the top.
