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This model defines the structure and applicability of aero dynamical complex data (up to four dimensions without flap influence which is separate considered) in steady states calculus for different configurations and optional cases (ground effect, asymmetrical propulsion (one of engines out) as well as in dynamic simulations.They user is offered many facilities of data entry, correction and graphical view. The punctual values of dimensional parameters for each coefficient are automaticaly checked for the string strictly increased or decreased specific feature.