The Polygon method of Woods is used to calculate the velocity distribution over a number of two-dimensional aerofoils at low incidence, subcritical flows only being considered. Lift slopes and aerodynamic centres at zero ...
The semi-empirical 'equivalent profile' method of W. P. Jones (1948) is extended to the case of an aerofoil with an oscillating control. The oscillatory hinge-moment derivatives for such an aerofoil-control combination in ...
Part I is an introduction to an empirical and theoretical study of two-dimensional aerofoil flows which include a limited region of supersonic flow terminated by a shock wave. A brief review of theoretical studies of the ...