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SparkJet EfficiencyA 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.
Document ID
20130003316
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Golbabaei-Asl, Mona
(Rutgers - The State Univ. New Brunswick, NJ, United States)
Knight, Doyle
(Rutgers - The State Univ. New Brunswick, NJ, United States)
Anderson, Kellie
(Rutgers - The State Univ. New Brunswick, NJ, United States)
Wilkinson, Stephen
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 27, 2013
Publication Date
January 7, 2013
Subject Category
Mechanical Engineering
Report/Patent Number
NF1676L-15877
AIAA Paper 2013-0928
Report Number: NF1676L-15877
Report Number: AIAA Paper 2013-0928
Meeting Information
Meeting: 51st AIAA Aerospace Sciences Meeting
Location: Grapevine, TX
Country: United States
Start Date: January 7, 2013
End Date: January 10, 2013
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: FA9550-10-1-011
WBS: WBS 694478.02.93.02.12.19.23
Distribution Limits
Public
Copyright
Public Use Permitted.
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