Inverse method with geometric constraints for transonic aerofoil design (Q3720139)

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Inverse method with geometric constraints for transonic aerofoil design
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    Inverse method with geometric constraints for transonic aerofoil design (English)
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    1986
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    Dirichlet boundary condition
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    Neumann boundary condition
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    design of aerofoils
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    pressure distribution
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    iterative procedure of 'residual- correction' type
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    finite-volume full-potential code
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    Corrections to the geometry
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    pressure residual
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    global, inverse, thin-aerofoil theory
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    local, inverse, wavy-wall theory
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    minimization problem
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