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Effects of Power Deposition on the Aerodynamic Forces on a Slender Body

2018; American Institute of Aeronautics and Astronautics; Volume: 56; Issue: 7 Linguagem: Inglês

10.2514/1.j057004

1533-385X

David Rodríguez-Gutiérrez, Jonathan Poggie,

Plasma and Flow Control in Aerodynamics

No AccessTechnical NoteEffects of Power Deposition on the Aerodynamic Forces on a Slender BodyDavid Rodríguez Gutiérrez and Jonathan PoggieDavid Rodríguez GutiérrezPurdue University, West Lafayette, Indiana 47907-2045 and Jonathan PoggiePurdue University, West Lafayette, Indiana 47907-2045Published Online:2 Apr 2018https://doi.org/10.2514/1.J057004SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About References [1] Bogdonoff S. M. and Vas I. E., "Preliminary Investigations of Spiked Bodies at Hypersonic Speeds," Journal of the Aerospace Sciences, Vol. 26, No. 2, 1959, pp. 65–74. doi:https://doi.org/10.2514/8.7945 LinkGoogle Scholar[2] Knight D. D., "Survey of Aerodynamic Drag Reduction at High Speed by Energy Deposition," Journal of Propulsion and Power, Vol. 24, No. 6, 2008, pp. 1153–1167. doi:https://doi.org/10.2514/1.24595 JPPOEL 0748-4658 LinkGoogle Scholar[3] Myrabo L. N. and Raizer Y. 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LinkGoogle Scholar Previous article Next article FiguresReferencesRelatedDetailsCited byHigh-speed aerodynamics control using energy injection of pulsed dischargesAerospace Science and Technology, Vol. 133Characterization of symmetric to non-symmetric flamefront transition in slender microchannelsProceedings of the Combustion Institute, Vol. 225Hypersonic drag and heat reduction mechanism of a new hybrid method of spike, multi-row discs and opposing jets aerodynamic configurationInternational Journal of Heat and Mass Transfer, Vol. 194An effective means of drag reduction in high enthalpy flow through unsteady energy depositionActa Astronautica, Vol. 186Universal scaling parameter for a counter jet drag reduction technique in supersonic flowsPhysics of Fluids, Vol. 32, No. 3Uncertainty and sensitivity study on blunt body's drag and heat reduction with combination of spike and opposing jetActa Astronautica, Vol. 167Charged particles distribution ahead the shock wave front in the electrode discharge plasmaJournal of Physics: Conference Series, Vol. 1400, No. 7 What's Popular Volume 56, Number 7July 2018 CrossmarkInformationCopyright © 2018 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the ISSN 0001-1452 (print) or 1533-385X (online) to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randp. TopicsAerodynamicsAeronautical EngineeringAeronauticsAirspeedCFD CodesComputational Fluid DynamicsEquations of Fluid DynamicsFlow RegimesFluid DynamicsFluid MechanicsNormal Shock WaveShock Waves KeywordsFreestream Mach NumberSlender BodyNonequilibrium FlowsKinetic EnergyIdeal GasBow ShockNumerical SimulationFlight ControlPlasma TorchesComputational Fluid Dynamics CodeAcknowledgmentsThe authors are grateful to A. Deshpande and K. Goc for assistance with the computations. Computer time was provided by Purdue University at the Rosen Center for Advanced Computing.PDF Received4 December 2017Accepted31 January 2018Published online2 April 2018