As seen in this picture, the tip vortices are said to make downwash. Why is that?
I’m also not sure why that’d tilt the lift vector backwards, but that might require a separate question.
Link to the article the picture is from.
As seen in this picture, the tip vortices are said to make downwash. Why is that?
I’m also not sure why that’d tilt the lift vector backwards, but that might require a separate question.
Link to the article the picture is from.
Your understanding is sophisticated enough that you shouldn't be trying to learn more from websites and other resources intended for pilots and laypersons. These resources do not apply sufficient rigor -- because rigor is not needed for that audience.
Instead, you should be learning from textbooks intended for engineers.
As you know, a wing can be represented by a horseshoe vortex system with a bound vortex at the quarter-chord line and two trailing vortices from the wingtips. These all have the same vorticity and can not exist without one another. Both the bound and trailing vortices contribute to downwash, but I think it is easiest to see how the bound vortex contributes.
I also personally do not like the description of induced drag tipping the lift vector backward -- lift is always perpendicular to the freestream. The total resultant aerodynamic force might be tipped backward, but not the lift vector.