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Characteristics of a Supersonic Fluidic Oscillator Using Design of Experiment

2020; American Institute of Aeronautics and Astronautics; Volume: 58; Issue: 6 Linguagem: Inglês

10.2514/1.j058968

1533-385X

Sanghoon Park, HeeChang Ko, MoonJung Kang, Yeol Lee,

Aerodynamics and Acoustics in Jet Flows

No AccessTechnical NotesCharacteristics of a Supersonic Fluidic Oscillator Using Design of ExperimentSangHoon Park, HeeChang Ko, MoonJung Kang and Yeol LeeSangHoon ParkKorea Aerospace University, Goyang 10540, Republic of Korea, HeeChang KoKorea Aerospace University, Goyang 10540, Republic of Korea, MoonJung KangAgency for Defense Development, Daejeon 34186, Republic of Korea and Yeol LeeKorea Aerospace University, Goyang 10540, Republic of KoreaPublished Online:22 Mar 2020https://doi.org/10.2514/1.J058968SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Cattafesta L. N. and Sheplak M., "Actuators for Active Flow Control," Annual Review Fluid Mechanics, Vol. 43, No. 1, 2011, pp. 247–272. https://doi.org/10.1146/annurev-fluid-122109-160634 CrossrefGoogle Scholar[2] Ostermann F., Woszidlo R., Nayeri C. N. and Paschereit C. 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TopicsAerodynamic PerformanceAerodynamicsAeronautical EngineeringAeronauticsBoundary LayersDesign of ExperimentsFlow RegimesFluid DynamicsFluid Flow PropertiesMechanical and Structural VibrationsMechanism and MachinesStructural Design and DevelopmentStructural EngineeringStructural Kinematics and DynamicsStructures, Design and TestVortex Dynamics KeywordsCentral Composite DesignsSweep AnglePower Spectral DensityIncompressible FlowProbability DistributionStagnation TemperatureAerodynamic DragResonance FrequenciesPressure SensorsImage ProcessingAcknowledgmentThe authors gratefully acknowledge the financial support provided by the Agency for Defense Development under the contract ADD-17-113-501-038.PDF Received16 August 2019Accepted25 February 2020Published online22 March 2020