Aspect-ratio effects in the driven, flux-core spheromak
dc.contributor.author | Hooper, E. B. | |
dc.contributor.author | Romero-Talamás, Carlos | |
dc.contributor.author | LoDestro, L. L. | |
dc.contributor.author | Wood, R. D. | |
dc.contributor.author | McLean, H. S. | |
dc.date.accessioned | 2024-01-24T10:53:26Z | |
dc.date.available | 2024-01-24T10:53:26Z | |
dc.date.issued | 2009-05-19 | |
dc.description.abstract | Resistive magnetohydrodynamic simulations are used to evaluate the effects of the aspect ratio (length to radius ratio) in a spheromak driven by coaxial helicity injection. The simulations are benchmarked against the Sustained Spheromak Physics Experiment (SSPX) [R. D. Wood et al, Nucl. Fusion 45, 1582 (2005)]. Amplification of the bias (“gun”) poloidal flux is fitted well by a linear dependence (insensitive to ) on the ratio of gun current and bias flux above a threshold dependent on A. For low flux amplifications in the simulations, the n = 1 mode is coherent and the mean-field geometry looks like a tilted spheromak. Because the mode has relatively large amplitude the field lines are open everywhere, allowing helicity penetration. Strongly driven helicity injection at A ≤ 1.4 in simulations generates reconnection events which generate cathode-voltage spikes, relaxation of the symmetry-breaking modes, and open, stochastic magnetic field lines; this state is characteristic of SSPX. The time sequences of these events suggest that they are representative of a chaotic process. Near the spheromak tilt-mode limit, A ≈1.67 for a cylindrical flux conserver, the tilt approaches 90°; reconnection events are not generated up to the strongest drives simulated. Implications for spheromak experiments are discussed. | |
dc.description.sponsorship | We thank the SSPX experimental team for their extensive efforts during the operation of the experiments. Stimulating discussions with B. I. Cohen are gratefully acknowledged, as is C. R. Sovinec’s help with the NIMROD code and spheromak physics, in general. The visualization in this work was made possible by the help of Brian Nelson at the PSI Center, University of Washington, who prepared the python code scripts which converted the NIMROD output into the proper format for VISIT. Brad Whitlock of LLNL provided much-needed consulting guidance on the use of VISIT, and W. H. Meyer of LLNL installed and debugged the code on a local computer system and provided important support as needed. The simulations made use of resources at the National Energy Research Supercomputer Center under Department of Energy Contract No. DE-AC03-76SF00098. The work was performed under the auspices of the U. S. Department of Energy by Lawrence Livermore National Laboratory under Contract Nos. W7405-ENG-48 and DE-AC52- 07NA27344. | |
dc.description.uri | https://pubs.aip.org/aip/pop/article-abstract/16/5/052506/677892/Aspect-ratio-effects-in-the-driven-flux-core?redirectedFrom=fulltext | |
dc.genre | journal articles | |
dc.identifier.citation | E. B. Hooper, C. A. Romero-Talamás, L. L. LoDestro, R. D. Wood, H. S. McLean; Aspect-ratio effects in the driven, flux-core spheromak. Phys. Plasmas 1 May 2009; 16 (5): 052506. https://doi.org/10.1063/1.3134064 | |
dc.identifier.uri | https://doi.org/10.1063/1.3134064 | |
dc.identifier.uri | http://hdl.handle.net/11603/31452 | |
dc.language.iso | en_US | |
dc.publisher | AIP | |
dc.relation.isAvailableAt | The University of Maryland, Baltimore County (UMBC) | |
dc.relation.ispartof | UMBC Mechanical Engineering Department Collection | |
dc.rights | This work was written as part of one of the author's official duties as an Employee of the United States Government and is therefore a work of the United States Government. In accordance with 17 U.S.C. 105, no copyright protection is available for such works under U.S. Law. | |
dc.rights | Public Domain Mark 1.0 | en |
dc.rights.uri | https://creativecommons.org/publicdomain/mark/1.0/ | |
dc.title | Aspect-ratio effects in the driven, flux-core spheromak | |
dc.type | Text | |
dcterms.creator | https://orcid.org/0000-0002-6830-3126 |