NASA NTRS · 20130003316
SparkJet Efficiency
Abstract
A novel method for determining the thermal efficiency of the SparkJet is proposed. A SparkJet is attached to the end of a pendulum. The motion of the pendulum subsequent to a single spark discharge is measured using a laser displacement sensor. The measured displacement vs time is compared with the predictions of a theoretical perfect gas model to estimate the fraction of the spark discharge energy which results in heating the gas (i.e., increasing the translational-rotational temperature). The results from multiple runs for different capacitances of c = 3, 5, 10, 20, and 40 micro-F show that the thermal efficiency decreases with higher capacitive discharges.
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Golbabaei-Asl, Mona, Knight, Doyle, Anderson, Kellie, Wilkinson, Stephen. 2013-01-07. SparkJet Efficiency. https://ntrs.nasa.gov/citations/20130003316
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