Numerical simulations of ICME–ICME interactions | Journal of Space Weather and Space Climate

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Fig. 12.

Same as Figures 8 and 10, but for the event of August 01, 2010. The closest model (shown in amber lines in the bottom two panels) is obtained reducing less than 35% the mass-loss rate of the CMEs, and less than 5% their initial speeds. The description of the figure is given in the text.

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