Abstract
The flow loss of a helical channel Magnetohydrodynamic (MHD) thruster without MHD effect was numerically studied with 3-D simulations, and a flow loss coefficient ζ was defined to quantify the flow loss and its influencing factors were studied. The results show that ζ decreases in a first-order exponential manner with the pitch of a helical wall and the Reynolds number, and it declines slowly when and t/T > 0.2 and Re > 105, a flow guide makes the flow more smooth and uniform, especially in the flow guide and helical wall sub-regions and thus reduces the flow loss greatly, by about 30% with the averaged value of ζ from 0.0385 to 0.027, a rectifier weakens the helical flow and strengthens the axial one in the rectifier and outlet sub-regions, thus reduces the rotational kinetic pressure with the averaged value of ζ declining about 4% from 0.0385 to 0.037, and ζ decreases with a rectifier’s axial length when Re > 105.
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Biography: ZHAO Ling-zhi (1977-), Female, Manchu, Ph. D. Candidate, Senior Engineer
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Zhao, Lz., Peng, Y., Lu, F. et al. 3-D Numerical Simulations of Flow Loss in Helical Channel. J Hydrodyn 24, 858–863 (2012). https://doi.org/10.1016/S1001-6058(11)60313-2
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DOI: https://doi.org/10.1016/S1001-6058(11)60313-2