
Thank you for the answers, guys.
That was exactly the discussion I read some weeks ago but I wasn’t able to find it again.
I also read that explanation but it left me with some doubts…
From my point of view I see a “normal” wing with a normal wing twist (bigger inner angles and lower outer angles) in order to have the correct stall response.
So what I expect is that Sidewinder missile on the external pylon is a little bit rotated down and it is normal that this effect is more evident on F-35A and B shorter wing.
The Sidewinder seems to be “parallel to its wing section” in order to cause a reduced drag to the airflow around it.
On C variant the Sidewinder pylon is farther away from the wingtip than on A and B and so it is also less rotated down.
In other words, more than with the angle of attack during the launch, I see a correlation between pylons and wing twist.
Or better…I see it for all pylons on C variant, but only for internal and external pylons on A e B variants.
The mid pylon on A and B variants is something that is not clear for me and if its “abnormal”angle (connected to the "spacer" highlighted in red in image below) is due to some reason about “safe separation”, it is not so evident for me how it exactly could solve the problem and why a bigger (but similar) wing on C version does not cause those separation problems or a so different air flow around the wing that requres that "spacer" on A and B.

That was exactly the discussion I read some weeks ago but I wasn’t able to find it again.
I also read that explanation but it left me with some doubts…
From my point of view I see a “normal” wing with a normal wing twist (bigger inner angles and lower outer angles) in order to have the correct stall response.
So what I expect is that Sidewinder missile on the external pylon is a little bit rotated down and it is normal that this effect is more evident on F-35A and B shorter wing.
The Sidewinder seems to be “parallel to its wing section” in order to cause a reduced drag to the airflow around it.
On C variant the Sidewinder pylon is farther away from the wingtip than on A and B and so it is also less rotated down.
In other words, more than with the angle of attack during the launch, I see a correlation between pylons and wing twist.
Or better…I see it for all pylons on C variant, but only for internal and external pylons on A e B variants.
The mid pylon on A and B variants is something that is not clear for me and if its “abnormal”angle (connected to the "spacer" highlighted in red in image below) is due to some reason about “safe separation”, it is not so evident for me how it exactly could solve the problem and why a bigger (but similar) wing on C version does not cause those separation problems or a so different air flow around the wing that requres that "spacer" on A and B.
