The physics of airplane flight
The article debunks the classic airfoil shape necessity for lift, explaining lift generation with any angled surface. It covers angle of attack, stalls, stability axes, speed, altitude, drag, and stalls' impact on wing airflow.
Read original articleThe article discusses the physics of airplane flight, debunking the misconception that wings must have a classic airfoil shape to generate lift. It explains how any surface angled upwards can create lift and function as a wing. The text delves into concepts like angle of attack, stalls, center of mass and pressure, stability in pitch, yaw, and roll axes, as well as speed stability. It also touches on the interaction of altitude and pitch stability, drag, and the phugoid oscillation phenomenon. The article emphasizes the importance of maintaining a constant angle of attack for flight stability and describes how a stall affects airflow over the wing. Overall, it provides a detailed insight into the aerodynamics and principles governing the flight of airplanes.
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I remember learning about it and wondering why newton's 3rd law wouldn't suffice. It's pretty obvious that the wings push air down and it's not that difficult to understand (even as a kid) that newton's 3rd law works.
The essence of the Bernoulli argument is that the top of the wing is longer -> air has to move further -> faster air has lower pressure "because Bernoulli" -> pressure imbalance means lift.
Ok, cool, but the "Bernoulli principle" I got as a kid was "faster air is lower pressure", which is both empirically wrong (the air in a compressor hose is obviously moving faster than the air in the workshop) and logically inconsistent (speed is relative, after all). You add in a half dozen qualifiers and it becomes true, but I wonder if this is more complicated than "the wings push air down, the air pushes the wing up".
>Additionally, a horizontal stabilizer in the back needs to be pitched down relative to the wings, creating downwards lift, pitching the plane up.
Naturally, this is a fundamental source of inefficiency.This is something I appreciate about the Lilium aircraft: they use canards to avoid this problem. Their latest design places the rear wing slightly above the canard[1], minimizing the downwash disadvantages[2] inherent in many canard configurations.
[1] https://www.youtube.com/watch?v=qZ73PftBfFg&t=273
[2] https://aviation.stackexchange.com/questions/83584/are-canar...
Is there a nice way to derive this? I find it interesting it's not the exact center though I guess it makes sense given the angle of the surface.
I parked it in my brain as something I didn't really understand and forgot about it. This was until not so many years ago when I found a satisfactory answer on YouTube. It was criminal to have been raised in an era without the internet.
Edit: added book title
Left unsaid is why aircraft wings have airfoil-shaped cross sections with cambered (concave-down) shapes: they produce more lift for a given wing loading and angle of attack.
This is why aircraft have flaps, as well. They increase the camber of the wing so that the pilot can fly slower without pitching the nose up, which is important for example when maintaining sight of the runaway on landing approach.
Wait, is it speeding up here or slowing down? Slowing down means deceleration, speeding up is acceleration, and it can't be doing both at the same time.
> When the plane slows down, it produces less drag, allowing to to pick up more speed.
Same deal?
I think what he's getting at is that drag increases with the square of speed, but it's a very confusing way of explaining it.
https://www.scientificamerican.com/video/no-one-can-explain-...
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