Flow Matching Results of an MHD Energy Bypass System on a Supersonic Turbojet Engine using the Numerical Propulsion System Simulation (NPSS) Environment-Reference-Cited by-同舟云学术

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

Published:2011-06-14 Issue: Volume: Page:
ISSN:
Container-title:42nd AIAA Plasmadynamics and Lasers Conference
language:
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Author:

Benyo Theresa¹

Affiliation:

1. NASA Glenn Research Center

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.2011-3591

Reference11 articles.

1. 2Benyo, T.L."InitialFlowMatchingResultsofMHDEnergyBypassonaSupersonicTurbojetEngineusingtheNumerical Propulsion SystemSimulation (NPSS) Environment", June2010,AIAA-2010-4301.

2. 4"NPSSUserGuide:SoftwareRelease:NPSS_1.6.5",NumericalPropulsionSystemSimulation NASAIndustryCooperative Effort, March 12,2008.

3. 5Jones, S. M. "An Introduction of Thermodynamic Performance Analysis of Aircraft Gas Turbine Engine Cycles Using the Numerical Propulsion SystemSimulation Code", NASATM-2007-214690, March2007.

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1. Multi-field coupling dynamic modeling and simulation of turbine test rig gas system;Simulation Modelling Practice and Theory;2014-05

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