In this report are collected together the calculated aerodynamic loadings due to incidence of a number of straight and swept-back wings. The calculations follow in the main the routine described previously in another report, ...

Stability and flutter derivatives are obtained for rectangular wings describing plunging and pitching oscillations in subsonic flow. These are evaluated by applying the simple approximate 'equivalent' wing theory (R. & M. ...

A method for the calculation of three-dimensional turbulent boundary layers is given. It depends on the assumptions that the component of the velocity in the boundary layer parallel to the external streamlines follows a ...