Subject: Lift Distribution along Wing versus Altitude

We know that Lift distribution along the wing is related to 
the aerofoil & wing shape. If we assume the case of a given wing (whichever) do 
you know what is the relationship between the lift distribution along the wing 
(from root to wing tip) and the altitude? How does the flying altitude
(barometric pressure) affects the lift distribution? I would appreciate any 
additional info. There is no answer to this question in your archive. Thank you 
in advance.

Re: Lift Distribution along Wing versus Altitude