High-Aspect-Ratio Wings in Steady Motion
摘要
WhilstHigh-aspect-ratio wings in steady motion a general closed-form solution for aerodynamic loads acting on a finite wing (rather than on its section as a part of the wing of infinite span) can be elusive, a limited asymptotic solution can often be constructed based on a small parameter characterizing the geometry of a particular wing. In this chapter they are found for a wing having its span large as compared with the chord.