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Conditionally Sampled Pulsejet Driven Ejector Flow Field Using DPIV

Presented at: 22nd AIAA Aerodynamic Measurement Technology & Ground Testing Conference, St. Louis, MO, June 24-26, 2002 (AIAA-2002-2321)

Authors: Wentworth T. John, Daniel E. Paxson and Mark P. Wernet

Digital Particle Imaging Velocimetry (DPIV) is a planar measurement technique, which enables the study of transient flows and significantly reduces facility test time. DPIV was used in the Glenn Research Center’s Rocket lab to characterize the high temperature, high speed flow field properties of a pulsejet coupled with an ejector of rectangular cross-section. Using a dynamic pressure transducer located in the pulsejet combustion chamber, the DPIV system was used to conditionally sample the flow field leaving the pulsejet and entering the ejector. The pulsejet driven ejector flow was sampled over a range of phase steps to completely map the operational cycle of the pulsejet. The instantaneous velocity maps obtained using DPIV were used to determine mean and fluctuating flow properties. These measurements will ultimately be used to properly validate the computational model predictions of the pulsejet driven ejector flow.



The PIV system installation in the PulseJet facility. The laser light sheet is brought in from above. Measurments were obtained both with and without the diffuser. A dual camera arrangement was used to record the complete flow field.






The Pulse Jet rig in operation. Run times do not exceed 15 seconds.




Animation of the complete pulse jet cycle. Note that air is sucked back into the pulse jet to start the next ignition cycle.

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Last Updated: 12/20/2005