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- W1979332291 abstract "The radiative heat flux incident on a re-entry body poses a significant challenge for spacecraft designers. With gas temperatures many time hotter than the sun, the physical mechanisms which determine the level and spectral detail of the radiation cannot yet be predicted with well defined uncertainty bounds, and more experimental data is required to improve and validate theoretical models. Ground testing facilities provide a means of doing this, but reproducing flight conditions on geometrically scaled flight models is only possible for a restricted range of circumstances. Specifically, it is not possible to simultaneously create embedded regions of equilibrium and non equilibrium thermo-chemistry in a scaled hypervelocity flow field which is correctly coupled with the radiant heat flux. This paper reports on a study to recreate a small region of equilibrium gas at the temperatures and pressures pertaining to the shock layers formed during hyperbolic earth entry, in order to make accurate radiation measurements at well defined flow conditions." @default.
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- W1979332291 date "2011-01-04" @default.
- W1979332291 modified "2023-09-23" @default.
- W1979332291 title "Simulation of Radiating Flows in Impulsive Facilities" @default.
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- W1979332291 doi "https://doi.org/10.2514/6.2011-250" @default.
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