Open Access
Fig. 11
Download original image
Variation of the mean rate of inertial energy dissipation per unit mass ϵ as a function of orbital phase Φ over the second and the third orbit. As in Fig. 8, the error bars indicate the standard deviation computed from six consecutive output flies, ϵ is given in units of с3 AU−1.
Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.
Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.
Initial download of the metrics may take a while.