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- W3176091245 abstract "Second- and third-order, noncentered finite-difference schemes are described for the numerical solution of the hyperbolic equations of fluid dynamics. The advantages of noncentered methods over the more conventional centered schemes are: simpler programming logic, nonhomogeneous terms are easily included, and generalization to multidimensional problems is direct. Second- and third-order methods are compared with regard to dissipative and dispersive errors and shock-capturing ability. These schemes are then used in a shock-capturing technique to determine the inviscid, supersonic flow field surrounding space shuttle vehicles (SSV). Resulting flow fields about typical pointed and blunted, delta-winged SSVs at angle of attack are presented and compared with experiment." @default.
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- W3176091245 date "1972-01-17" @default.
- W3176091245 modified "2023-09-27" @default.
- W3176091245 title "Computation of space shuttle flow fields using noncentered finite-difference schemes" @default.
- W3176091245 doi "https://doi.org/10.2514/6.1972-193" @default.
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