Title: Effect of leakage past aileron nose on aerodynamic characteristics of plain and internally balanced ailerons on NACA 66(215)-216, a = 1.0 airfoil
Description: <a href="http://uf.catalog.fcla.edu/uf.jsp?st=UF003807484&ix=nu&I=0&V=D&pm=1" rel="nofollow">http://uf.catalog.fcla.edu/uf.jsp?st=UF003807484&ix=nu&I=0&V=D&pm=1</a>
Subjects: Ailerons, Aerodynamics--Research.