Initial Flow Matching Results of MHD Energy Bypass on a Supersonic Turbojet Engine Using the Numerical Propulsion System Simulation (NPSS) Environment

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• 来源
  《AIAA Fluid Dynamics Conference and Exhibit;AIAA/ASME Joint Thermophysics and Heat Transfer Conference;AIAA CFD High-Lift Prediction Workshop;HILIFTPW-1;AIAA Aerodynamic Measurement Technology and Ground Testing Conference;AIAA Applied Aerodynamics Conference;Plasmadynamics and Lasers Conference;Flow Control Conference》|2010年|P.1-12|共12页
• 会议地点 Chicago, IL(US);Chicago, IL(US);Chicago, IL(US);Chicago, IL(US);Chicago, IL(US);Chicago, IL(US);Chicago, IL(US);Chicago, IL(US)
• 作者

  T. Benyo;

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• 作者单位

  NASA Glenn Research Center Cleveland OH;

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