A new method for the aerodynamic analysis of lifting surfaces

The use of the original Ffowcs Williams and Hawkings equation to improve the solution to simple problems of two-dimensional and incompressible flow is studied. It is shown that a linear formulation, with the quadrupole term neglected, leads to better correlation with the results of potential theory. A solution to steady and two-dimensional problems is developed and applied to families of elliptic cylinders and symmetric airfoils.