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Efficiency of SparkJetThe thermal efficiency of a SparkJet is evaluated by measuring the impulse response of a pendulum subject to a single spark discharge. The SparkJet is attached to the end of a pendulum. A laser displacement sensor is used to measure the displacement of the pendulum upon discharge. The pendulum motion is a function of the fraction of the discharge energy that is channeled into the heating of the gas (i.e., increasing the translational-rotational temperature). A theoretical perfect gas model is used to estimate the portion of the energy from the heated gas that results in equivalent pendulum displacement as in the experiment. The earlier results from multiple runs for different capacitances of C = 3, 5, 10, 20, and 40(micro)F demonstrate that the thermal efficiency decreases with higher capacitive discharges.1 In the current paper, results from additional run cases have been included and confirm the previous results
Document ID
20140000598
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Golbabaei-Asl, M.
(Rutgers - The State Univ. New Brunswick, NJ, United States)
Knight, D.
(Rutgers - The State Univ. New Brunswick, NJ, United States)
Wilkinson, S.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
February 7, 2014
Publication Date
July 1, 2013
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NF1676L-16630
Report Number: NF1676L-16630
Meeting Information
Meeting: European Conference for Aeronautics and Space
Location: Munich
Country: Germany
Start Date: July 1, 2013
End Date: July 5, 2013
Funding Number(s)
CONTRACT_GRANT: FA9550-10-1-0111
WBS: WBS 794072.02.07.02.02
CONTRACT_GRANT: SAA1-1360
Distribution Limits
Public
Copyright
Public Use Permitted.
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