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- W1966964051 abstract "The ability of the current Nusselt number prediction technique developed by Kavanau (1955) to accurately predict alumina particle heat transfer rates in solid rocket nozzles and plumes is investigated. For the solid rocket motors SRMS) analyzed, the transitional regime is the dominant regime for the majority of particles in the flowfield. The analytical approach to determine accuracy of the Kavanau correlation utilized the G2R Direct Simulation Monte Carlo code. With this method, both sphere drag, and heat transfer rates were predicted. The sphere drag prediction were compared to the Hermsen, and Henderson drag correlations, while the heat transfer results were compared to the current theory. Results have indicated, that the predicted drag coefficient is bounded by the drag correlations considered. However, the Nusselt number varies significantly from the extrapolated profile through all flowfield regimes." @default.
- W1966964051 created "2016-06-24" @default.
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- W1966964051 date "1992-07-06" @default.
- W1966964051 modified "2023-09-26" @default.
- W1966964051 title "Investigation of gas/particle heat transfer rates in solid rocket motors" @default.
- W1966964051 doi "https://doi.org/10.2514/6.1992-3619" @default.
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