Development of a method for predicting wing pressure distributions in subsonic flow: report on an intermediate solution

A method is described for predicting pressure distributions on wings in subcriticial attached flow. The method comprises the following basic elements. - linearized lifting surface theory the surface source panel method of Hess and Smith - approximate, uniformly valid, second-order corrections to be applied to the results of lifting surface...

A digital computer programme for predicting pressure distributions on swept wings in subsonic flow according to a semi-empirical method

A computer programme is presented for the application of a semi-empirical method, based on work from the Royal Aircraft Establishment, for calculation of the pressure distribution on wings in subsonic attached flow. A comparison of calculated results with results of experiments is made with the purpose to determine some of the boundaries of the...