Titlebook: Recent Development of Aerodynamic Design Methodologies; Inverse Design and O Kozo Fujii,George S. Dulikravich Book 1999 Springer Fachmedien

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Application of Transonic Inverse Method to the Development of Aerospace Products,en the specified and computed pressure distribution, starting from a baseline geometry..This paper shows two applicated examples of this inverse problem. One is for swept wing of typical civil transport. The other is for non-planar wing of H-II Orbiting Plane(HOPE) tipfin configuration.

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Multi Objective Aerodynamic Optimisation by Means of Robust and Efficient Genetic Algorithm,thodologies the operators considered at present the most promising one are described. A simple mathematical test is used for preliminary algorithmic perfomance while in more applicative cases the pressure reconstruction problem of two conflicting aerodynamic profiles is used as benchmark. A full pot

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Subsonic Aerodynamic Design Via Optimization,of attack. Effects of flaps deflection can be incorporated and the induced drag can be minimized. A higher order panel method is applied to perform flow analysis. Flaps deflection is simulated by modifying a Neumann boundary conditions. In the design case the geometry which minimizes differences bet

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Numerical Methods for Inverse Solution in Aerodynamic Design of Turbomachinery,function(SF) method of two different kinds of stream surfaces, which are usually assumed for the design in turbomachinery, stream-function-coordinate(SFC) method for two-dimensional and three-dimensional flows, potential function(PF) method and the method based on the direct solution with a residual

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Inverse Blade Design Based on Permeable Wall Concept,ed how the permeable wall concept can be used to define the blade modifications required to obtain the target performances with a small number of iterations. It is shown how the method can be combined with potential flow methods, Euler and Navier Stokes solvers. Each method is illustrated with examp