Sparkjet Development, Characterization, and Initial Implementation into a Supersonic Boundary Layer
Active flow control actuators have been studied rigorously by the aerodynamic community and developments have led to a wide variety of devices with various features and operating mechanisms. The design requirements for a practical actuator used for active flow control include reliable operation, req...
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| Format: | Others |
| Language: | English English |
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Florida State University
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| Online Access: | http://purl.flvc.org/fsu/fd/FSU_migr_etd-7368 |