Jul 2 – 6, 2018
Žofín Palace
Europe/Prague timezone

O2.109 L-H transition dynamics with applied n=3 resonant magnetic perturbations

Jul 3, 2018, 12:10 PM
15m
Small Hall

Small Hall

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Speaker

Lothar Schmitz

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See the full Abstract at http://ocs.ciemat.es/EPS2018ABS/pdf/O2.109.pdf L-H Transition Dynamics with Applied n=3 Resonant Magnetic Perturbations* L. Schmitz,1 M. Kriete,2 R. Wilcox,3 Z. Yan,2 T.L. Rhodes,1 C. Paz-Soldan,4 A. Marinoni,5 G.R. McKee,2 P.Gohil,4 L. Zeng,1 and C.C. Petty.4 1 University of California-Los Angeles, Los Angeles, CA 90095-7799, USA 2 University of Wisconsin-Madison, Madison, WI 53706, USA 3 Oak Ridge National Laboratory, Oak Ridge, TN 37831-0117, USA 4 General Atomics, PO Box 85608, San Diego, CA 92186-5608, USA 5 PFSC, Massachusetts Institute of Technology, Cambridge, MA 02139, USA In ITER-similar plasmas in DIII-D (=1.5- 5x1019m-3, Bt=1.9-2T, Ip=1.5MA, q95~3.6), the L-H threshold power PLH with n=3 Resonant Magnetic Perturbations (RMP) is found to increase strongly with decreasing collisionality, a concern for H-mode access in primarily ECH-heated ITER plasmas since RMP may be applied before the L-H transition in ITER to safely suppress the first ELM. Low edge collisionality is thought to lead to substantial additional thermal losses across the last closed flux surface in ITER, potentially increasing the L-H power threshold [1]. Figure 1 clearly shows that PLH increases at low collisionality, and that the collisionality dependence of PLH is much more Fig. 1: L-H transition power threshold PLH pronounced with applied RMP [PLH~(ν*)-0.3] vs. collisionality ν* (ρ = 0.95) without and compared to non-RMP plasmas [PLH~(ν*)-0.1]. with applied n=3 RMP (3.3×10-4 ≤ δB/B ≤ -4 Pronounced non-axisymmetric modifications of the 4.6×10 The expected ITER L-mode edge collisionality range is shaded. L-mode shear layer with RMP include a substantial local reduction of the Er well and ExB shear [in particular the outboard ExB shear layer is locally “eroded” for flux tubes connecting to high I-coil perturbation field]. Two-fluid modeling with the M3D-C1 code [2] shows that the normalized radial density gradient a/Ln is toroidally modulated and periodically increased on the outboard midplane with RMP. Low- wave-number turbulence is spatially modulated with RMP and increases substantially in amplitude on field lines connecting to high RMP perturbation field. We conjecture that the increase in PLH with RMP results from the combined effects on locally enhanced instability drive (via increased normalized density gradient) and reduced ExB shear. Theoretically, increased Reynolds stress would be required to initiate the L-H transition with RMP active [3], as the Reynolds stress [4] is counteracted by radial forces related to the RMP field structure. The observed increase of the L-H power threshold may be consistent with this picture, as the observed local turbulence increase with applied RMP may not substantially increase the flux-surface-averaged Reynolds stress. Non-resonant n=3 perturbations do not affect PLH significantly, and the modifications in turbulence level and ExB shear are minimal. [1] F. Ryter et al. Nucl. Fusion 54 083003 (2014). [2] R.S. Wilcox et al. Nucl. Fusion 57 116003 (2017). [3] M. Leconte et al, Nucl. Fusion 54 013004 (2014); G. Choi and T.S. Hahm, Nucl. Fusion 58 026001 (2018). [4] Z.Yan et al. Nucl. Fusion, 57, 126015 (2017); Z. Yan, et al. Phys Rev. Lett. 107, 055004 (2014). *This work was supported by the US Department of Energy under DE-FG02-08ER54984, DE-FG02- 89ER53296, DE-FG02-08ER 54999, and DE-FC02-04ER54698.

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