Rolling friction and lift in airplanes
I need some enlightenment on this question that am not clearly able to think about in the last few hours so. I believe someone here can help me discussing this-
When an airplane takes-off , there is this lift force(generated by maintaining an angle of attack and certain velocity and hence generating it through Bernoulli's principle) which plays a key role. The fact pestering me here is when the company deisgns an airplane, lets say a 8-wheeler or a 16 or 32 or whatever it is (excluding the nose landing one), Do they consider the rolling friction caused by these as it gains some speed and hence its effect on the velocity and force required for lift?
I am sure that this happens. Well, so could someone help me with an FBD on how it would look with these forces considered. What is the Frictional force made up of in this case ? just a vector going in the opposite direction or something more ?