Obtain the time dependent but steady lift coefficient, Eq. 8.48, and the boundary layer edge velocity, Eq. 8.49 for a chordwise flexible parabolically cambered thin airfoil whose equation is given by Eq. 8.46 and maximum camber location along the chord is given by \(p\).

Eq. 8.48

Eq. 8.49

Eq. 8.46

Transcribed Image Text:

w(x,t) = - [2ap(x-p)/(1+p) +2a(x p)(p U)/(1+p), x