Toward a High-Frequency Pulsed-Detonation Actuator
Author:
Affiliation:
1. George Washington University
2. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-555
Reference13 articles.
1. Funk,R.,Parekh,D.,Crittenden,T.andGlezer,A."TransientSeparationControlusingPulseCombustion Actuation,"AIAAPaper2002-3166,1stFlowControlConference,St.Louis,MO,24-26June2002.
2. NASALangleyResearchCenter,FactSheet#FS-2000-06-52-LaRC.
3. Crittenden,T.andGlezer,A.,Funk,R.,Parekh,D."Combustion-DrivenJetActuatorsforFlowControl,"AIAA2001-2768,31stAIAAFluidDynamicsConference&Exhibit,Anaheim,CA,11-14June2001.
4. Rinehart,C.,McMichael,J.M.,andGlezer,A."TransitoryFlowandForceDevelopmentonaBodyofRevolution Using SyntheticJetActuation,"AIAA-2003-0618,41stAerospaceSciencesMeetingandExhibit,Reno,NV,Jan.6-9,2003.
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