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- W2036763205 abstract "The problem of unsteady, supersonic, locally conical, vortical flow around a delta wing undergoing thickening oscillation is solved using the unsteady, thin-layer Navier-Stokes equations and the unsteady linearized Navier-displacement equations. The unsteady, thin-layer Navier-Stokes equations are solved using the implicit approximate-factorization finite-volume scheme to compute the conservative components of the flow vector field. With the conservative components known at any time step, the linearized, Navier-displacement equations are solved using the alternating, direction-implicit scheme to obtain the grid points displacements due to known displacement boundary conditions. A grid-displacements limiter, in the form of a low mesh Reynolds number, is used to limit grid-folding in regions of highly reversed flow." @default.
- W2036763205 created "2016-06-24" @default.
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- W2036763205 date "1989-08-14" @default.
- W2036763205 modified "2023-09-23" @default.
- W2036763205 title "Thickening oscillation of a delta wing using Navier-Stokes and Navier-displacement equations" @default.
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- W2036763205 doi "https://doi.org/10.2514/6.1989-3373" @default.
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