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Fluidic thrust shock-vector control is a promising new concept for steering rocket engines. We conduct a sensitivity analysis to quantify the impacts of main flow variables on the deflection angle. We find that estimation of the injector location and shocks position is of critical importance.
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This page is a summary of: Fluidic Thrust Shock-Vectoring Control: A Sensitivity Analysis, AIAA Journal, April 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j058922.
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