- Joined
- May 1, 2008
- Messages
- 109
- Reaction score
- 2
A plane flies from low to high altitude at constant velocity. Which of the following is true?
The passage says:
"Bernoulli's equation, P + 1/2ρv2 + ρgh = constant, is often modified when discussing an airplane's wing. The "ρgh" component is usually left out since the difference in distance from the top of the wing to the ground compared to the bottom of the wing to the ground is usually negligible."
What I was thinking was that the pgh term in Bernoulli's only accounted for the difference in height between the top and bottom of the wing. The reason is because the 'P' that we ultimately care for is actually the deltaP between the top and bottom of the wing, for that is what causes lift.
I'm not sure what the the answer explanation is talking about... even if the absolute P changes, how does that change how much lift a wing has? That would mean just because an airplane is flying at a lower altitude, it should have more lift (assuming it is flying at the same velocity as an airplane flying at a higher altitude).
Huh?
- At the lower altitude the plane will experience greater lift. A
At the higher altitude the plane will experience greater lift B
The lift the plane experiences is not dependent on altitude. C
At low altitudes Bernoulli's effect is not applicable. D
The passage says:
"Bernoulli's equation, P + 1/2ρv2 + ρgh = constant, is often modified when discussing an airplane's wing. The "ρgh" component is usually left out since the difference in distance from the top of the wing to the ground compared to the bottom of the wing to the ground is usually negligible."
What I was thinking was that the pgh term in Bernoulli's only accounted for the difference in height between the top and bottom of the wing. The reason is because the 'P' that we ultimately care for is actually the deltaP between the top and bottom of the wing, for that is what causes lift.
I'm not sure what the the answer explanation is talking about... even if the absolute P changes, how does that change how much lift a wing has? That would mean just because an airplane is flying at a lower altitude, it should have more lift (assuming it is flying at the same velocity as an airplane flying at a higher altitude).
Huh?