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A SparkJet actuator is a promising flow control device. We present analytic model for the actuator to predict and estimate its performances, such as thrust, impulse and velocity at the orifice. This developed model has improved accuracy over others.
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This page is a summary of: Development of One-Dimensional Analytical Model for a SparkJet Actuator, AIAA Journal, March 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059619.
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