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- W2107834675 abstract "The benefits of introducing an advanced disc sizing criterion in the application of high and low pressure turbines of high speed engines are evaluated. The criterion used to size the turbine disc accounts for loads on the blade. Results from a linear elastic structural analysis of a high pressure turbine disc are presented. The implementation of the turbine disc sizing criterion in the Engine Structures Technology Benefit Estimator code (EST/BEST) produced significant reduction in the weight of high and low pressure turbine. The overall engine weight is reduced by 4.5%. Benefits in the areas of weight, mission, cost, and maintenance obtained with the use of the disc sizing criterion are described in this paper." @default.
- W2107834675 created "2016-06-24" @default.
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- W2107834675 date "1998-04-20" @default.
- W2107834675 modified "2023-09-26" @default.
- W2107834675 title "Benefits of advanced disc sizing criterion for engines of high speed aircraft" @default.
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- W2107834675 doi "https://doi.org/10.2514/6.1998-1759" @default.
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