The surface analysis of hovercraft

Bearing surfaces W.I.G. craft the any form are investigated. Values of aerodynamic factors су(α, h) and mz(α, h), relative coordinate of aerodynamic focus xf (α, h), distribution of aerodynamic loading on a bearing surface for three forms of bearing surfaces are received numerical. Functional dependences сy = f(α, h), mz = f(α, h), xf = (α, h) are constructed.