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- W2186471180 abstract "Interest in fluidic thrust vectoring has promoted many numerical and experimental investigations to explore its validity in real world applications. The benefits of such technology are numerous making investigations into their effectiveness a valid and worthwhile exercise. A comprehensive literature review of previous work was conducted from which an appropriate numerical simulation criterion was devised. This was carried out to replicate experimental results and in-turn validate two dimensional computational fluid dynamic simulations using FLUENT® as an appropriate method of investigation. Specifically the method of fluidic thrust vectoring using the technique of shock vector control will be used. Numerical simulations conducted aim to replicate previous experimental work by Stagg (2008), using the Australian Defence Force Academy fluidic thrust vectoring experimental apparatus, and Neely et al (2007). Following initial CFD validations a numerical exploration of fluidic thrust spoiling as a means of thrust magnitude control in solid fuel rocket motors will be conducted. Results obtained from computational fluid dynamics simulations will be then used to develop a suitable control system for both thrust magnitude and direction will be carried out." @default.
- W2186471180 created "2016-06-24" @default.
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- W2186471180 date "2009-09-08" @default.
- W2186471180 modified "2023-09-23" @default.
- W2186471180 title "Numerical investigation of Fluidic Injection as a means of Thrust Modulation" @default.
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