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Power Requirement for Nonequilibrium MHD-Bypass ScramjetIt has been suggested previously that the performance of scramjet propulsion system may be improved by the use of magnetohydrodynamic (MHD) energy bypass: an MHD generator could be made to decelerate the flow entering the combustor, thereby improving combustion efficiency, and the electrical power generated could be made to accelerate the flow exiting from the combustor prior to expanding through the nozzle. In one of such proposed schemes, the MHD generator is proposed to be operated at a low temperature and ionization is to be achieved under nonequilibrium by the application of an external power. In the present work, the required power of such an external source is calculated assuming a 100%-efficient nonequilibrium ionization scheme. The power required is that needed to prevent the degree of ionization from reaching equilibrium with the low gas temperature. The flow is seeded with potassium or cesium. Specific impulse is calculated with and without turbulent friction. The results show that, for typical intended flight conditions, the specific impulse obtained is substantially higher than that of a typical scramjet, but the required external-power is several times that of the power generated in the MHD generator.
Document ID
20010066491
Acquisition Source
Ames Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Park, Chul
(Eloret Corp. United States)
Bogdanoff, David W.
(Eloret Corp. United States)
Mehta, Unmeel
(NASA Ames Research Center Moffett Field, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: 39th AIAA Aerospace Sciences Meeting
Location: Reno, NV
Country: United States
Start Date: January 1, 2001
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
PROJECT: RTOP 242-74-10
CONTRACT_GRANT: NAS2-99092
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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