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The Effect of Magnetohydrodynamic (MHD) Energy Bypass on Specific Thrust for a Supersonic Turbojet EngineThis paper describes the preliminary results of a thermodynamic cycle analysis of a supersonic turbojet engine with a magnetohydrodynamic (MHD) energy bypass system that explores a wide range of MHD enthalpy extraction parameters. Through the analysis described here, it is shown that applying a magnetic field to a flow path in the Mach 2.0 to 3.5 range can increase the specific thrust of the turbojet engine up to as much as 420 N/(kg/s) provided that the magnitude of the magnetic field is in the range of 1 to 5 Tesla. The MHD energy bypass can also increase the operating Mach number range for a supersonic turbojet engine into the hypersonic flight regime. In this case, the Mach number range is shown to be extended to Mach 7.0.
Document ID
20110002743
Document Type
Technical Memorandum (TM)
Authors
Benyo, Theresa L.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
December 1, 2010
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
E-17311
AIAA Paper-2010-232
NASA/TM-2010-216734
Meeting Information
AIAA 48th Aerospace Sciences Meeting and Exhibit(Orlando, FL)
Funding Number(s)
WBS: WBS 599489.02.07.03.04.03.01
WBS: WBS 599489.02.07.03.07.02.04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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