the Choloy war cemetery in France after the war. Many tributes were paid to Kain by the world’s media. Popular with his fellow airmen, he had shown himself to be a combat pilot of remarkable skill, and had achieved almost legendary status in the early months of the war.pressure field. A marching computational method was later implemented starting at the known upstream boundary condition. The stagnation pressure of the incoming flow from the upstream boundary was adjusted at every spatial location by integrating the change in stagnation pressure caused by work addition/subtraction evident through the corresponding velocity gradient. Once this was obtained, the static pressure field was extracted simply as the difference between the stagnation pressure and the local dynamic pressure as obtained from the magnitude of the local velocity vector. This work was further extended to include the viscous terms by solving the incompressible 2D Navier Stokes equations.

Two approaches were used in this method. The first involved viscous terms being added iteratively as correction terms to the assumed Bernoulli pressures in the entire flowfield. The