Computer programs have been written to evaluate the integrals of lifting-surface theory for the velocity field of a thin wing with given load distribution. Different programs are used for the downwash at points on the wing, ...
A method for the calculation of the section thickness distribution to produce a given symmetrical pressure distribution near the critical Mach number is presented. By linearisation about a known solution, obtained by Sells' ...
A pilot method has been developed, and an EMA computer program written, for the iterative calculation of the load distribution on a thin wing with prescribed warp (downwash). At each iteration the downwash due to the current ...
A method of computing the steady, inviscid flow around a thick, cambered and twisted wing (neglecting dihedral) is presented. The flow field is represented by distributions of sources and doublets in the chordal surface, ...
A computer programme has been written to solve the steady laminar two-dimensional boundary-layer equations for a perfect gas at given wall temperature, without wall suction. The programme solves the equations at a blunt ...