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- W4205664971 abstract "Supersonic retropropulsion was simulated using an Euler solver in an axisymmetric domainto investigate the unsteady motions of the flow features caused by interaction between the freestream and retropropulsion jet. Thrust coefficients between 0.140 and 0.600 were simulated,and two different jet gases, into ambient nitrogen, were studied. The first was nitrogen witha stagnation temperature equal to that of the free stream, corresponding to past experimentsperformed by the authors. At high thrust coefficients above C_T=0.17, a longitudinal oscillationin the bow shock position at about 8 kHz was observed in the simulations, which agrees closelywith the experiments at the same thrust coefficient value. At lower thrust coefficients, the modesobserved in experiments were not reproduced in the simulations, indicating that the modes aremost likely not axisymmetric. The second jet gas was hot water vapor to simulate combustionproducts. Even at high thrust coefficients, the dual-gas cases resulted in flows with no distinctoscillatory modes, and the flow field was dominated by low frequency, large magnitude motionsof the flow features." @default.
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- W4205664971 date "2022-01-03" @default.
- W4205664971 modified "2023-09-28" @default.
- W4205664971 title "Numerical Investigation of Aerodynamic Interference in Supersonic Retropropulsion" @default.
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- W4205664971 doi "https://doi.org/10.2514/6.2022-1180" @default.
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