DocumentCode :
2502265
Title :
Numerical simulation for hypersonic vehicle on-board magnetohydrodynamic power generation
Author :
Harada, Nob ; Kikuchi, Takashi ; Lineberry, John T.
Author_Institution :
Dept. Electr. Eng., Nagaoka Univ. of Technol., Nagaoka
fYear :
2008
fDate :
1-3 Dec. 2008
Firstpage :
828
Lastpage :
833
Abstract :
As one of the practical application of magnetohydrodynamic (MHD) electric power generation, hypersonic vehicle electric power system (HVEPS) program started from 2001. Scramjet driven MHD power generation experiments were conducted and reasonable output electric power was successfully extracted. We carried out 1- and 3-dimensional numerical simulations in order to explain experimental results. To predict inlet conditions precisely, we had to assume adequate combustion efficiency in the scramjet combustor. Hall potential distribution in the main part of generator channel agreed well with 1-d results using adequate non-uniformity G-factor. Although end effects could be explained by the 3-d simulation, effect of non-uniformity must be studied further.
Keywords :
aircraft; aircraft power systems; electric power generation; jet engines; magnetohydrodynamic convertors; missiles; numerical analysis; hypersonic vehicle electric power system; hypersonic vehicle on-board magnetohydrodynamic power generation; magnetohydrodynamic electric power generation; numerical simulation; scramjet engines; Combustion; Electric vehicles; Engines; Magnetic fields; Magnetohydrodynamic power generation; Numerical simulation; Plasma temperature; Power generation; Power system simulation; Test facilities; MHD generator; Magnetohydrodynamics; Scramjet engine; on-board power system;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Power and Energy Conference, 2008. PECon 2008. IEEE 2nd International
Conference_Location :
Johor Bahru
Print_ISBN :
978-1-4244-2404-7
Electronic_ISBN :
978-1-4244-2405-4
Type :
conf
DOI :
10.1109/PECON.2008.4762588
Filename :
4762588
Link To Document :
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