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Thanks to modern advances, the solution to an expression like Eq. 97b is almost
trivial (unless you are an arts student.) and does not require nearly the effort it used to.
Indeed, it is likely that most of you, as students famil
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So far we have discussed the pitching moment of the wing without regard to its stability.
However, if a cambered wing produces a pitching moment then clearly it will be unstable on an aircraft
without some sort of balancing force.
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From our analysis of the factors that influence an aircraft's roll characteristics, it is
clear we are reaching the limits of what can be done without considering dynamic effects.
Even if we decide to assume a roll created by an
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Having seen the elevator's effectiveness in altering the longitudinal trim conditions, it stands to
reason that it would also be effective in any other type of longitudinal manoeuvre, even when L W.
In order to consider these scenarios l