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- W2334790092 abstract "Rocket nozzles which feature amelioration of asymmetric flow separation and accompanying side-loads offer significant gains in vehicle safe life and launch efficiencies. Whilst this subject has been the purpose of much academic and industrial research the origins of such side-loads are still not well understood. It is believed that nozzle wall angle has been overlooked as a governing factor of flow separation stability. In order to explore this, an experimental programme examining the flow structure of subscale conical nozzles with wall angles of 8.3 ◦ , 10.4 ◦ and 12.6 ◦ is in progress at the University of Bristol. The ultimate aim of the programme is to develop a simple bell-type nozzle which features atmospheric adaption. This paper outlines the initial stages in the programme and presents preliminary data and analysis methodologies." @default.
- W2334790092 created "2016-06-24" @default.
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- W2334790092 date "2010-07-25" @default.
- W2334790092 modified "2023-09-26" @default.
- W2334790092 title "The Impact of Wall Angle on Nozzle Separation Behavior" @default.
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- W2334790092 doi "https://doi.org/10.2514/6.2010-7168" @default.
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