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- W2330475565 abstract "Flow unsteadiness is a major factor in turbine performance and durability. This is especially true if the turbine is a high work design, compact, transonic, supersonic, counter rotating, or uses a dense drive gas. The vast majority of modern rocket turbine designs fall into these categories. In this study a parallelized unsteady quasi-three-dimensional Navier-Stokes analysis has been combined with a genetic optimization algorithm to improve the performance of a supersonic turbine stage. NOMENCLATURE a - Speed of sound c - Axial chord m - Mass flow rate M - Mach number P - Static pressure t - Time T - Static temperature W - Work a - Absolute circumferential angle" @default.
- W2330475565 created "2016-06-24" @default.
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- W2330475565 date "2000-09-06" @default.
- W2330475565 modified "2023-09-26" @default.
- W2330475565 title "Multi-objective shape optimal design of a supersonic turbine" @default.
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- W2330475565 doi "https://doi.org/10.2514/6.2000-4860" @default.
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