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- W2027142 abstract "Publisher Summary In recent years, substantial progress has been made in the development of efficient algorithms for solving discrete approximations to the potential equation for transonic flow past rather general geometrical configurations. This chapter describes the approximations implicit in the potential formulation and some of the difficulties associated with computing the flows past complicated geometric shapes. The geometrical complexity of problems solvable with a reasonable expenditure of computer resources varies inversely with the degree of fluid-mechanical complexity required to model the important features of the flow field. The ultimate goal of computational aerodynamicists is to solve the Navier-Stokes equations for a complete aircraft configuration, consisting of wing, fuselage, tail, nacelles, etc. The solution of the resulting Navier-Stokes equations presents a formidable problem, especially when the Reynolds number is high so that the length scales relevant to the parabolic terms and to the convective terms become widely disparate." @default.
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- W2027142 date "1982-01-01" @default.
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- W2027142 title "Calculation of Transonic Potential Flow Past Three-Dimensional Configurations" @default.
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- W2027142 doi "https://doi.org/10.1016/b978-0-12-493280-7.50009-7" @default.
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