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- W2989056554 abstract "The impact of the gas-phase ionization on flow and surface properties at nonequilibrium hypersonic conditions is examined with the direct simulation Monte Carlo method for five-, seven-, and 11-species air models. The freestream velocity is varied from 6 to , and the Knudsen number is varied from 0.0003 to 0.0012. Validation is conducted for a normal shock wave and Radio Attenuation Measurement C Band (RAM-C) sphere–cone configuration. The model analysis is performed for a RAM-C forebody. Ionization is shown to noticeably change flow properties inside the shock at velocities of and higher, as well as in the boundary layer at velocities of and higher. The seven-species model is generally applicable up to . For higher velocities, it differs significantly from the 11-species model, especially inside the boundary layer; and it underpredicts the heat flux reduction due to ionization by a factor of two. Compared to the five-species model, the maximum change in the heat flux is 2% for the seven-species model and 4% for the 11-species model." @default.
- W2989056554 created "2019-11-22" @default.
- W2989056554 creator A5084698431 @default.
- W2989056554 creator A5087080425 @default.
- W2989056554 date "2020-03-01" @default.
- W2989056554 modified "2023-09-27" @default.
- W2989056554 title "Impact of the Ionization Reaction Set in Nonequilibrium Hypersonic Air Flows" @default.
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- W2989056554 doi "https://doi.org/10.2514/1.j058895" @default.
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