Jump Shocks in Molecular Clouds - Speed Limits and Excitation Levels

Details Jump Shocks in Molecular Clouds - Speed Limits and Excitation Levels Jump Shocks in Molecular Clouds - Speed Limits and Excitation Levels

Jan 1994

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1994mnras.266..238s&link_type=abstract

Monthly Notices of the Royal Astronomical Society, Vol. 266, NO. 1/JAN, P. 238, 1994

Astronomy and Astrophysics

Astronomy

76

Molecular Processes - Shock Waves - Ism: Clouds - Ism: Jets And Outflows - Ism: Molecules

Scientific paper

Below a speed limit, hydromagnetic jump shocks propagate through the interstellar medium without dissociating the molecules. The resulting excitation of the molecules is modelled here, where several factors, including the shock shape and magnetic field strength (i.e. the Alfvén speed), are explored. The speed limit for molecular hydrogen is in the range ˜24-39 km s-1 for low Alfvén speeds but reaches 50 km s-1 for an Alfvén speed of 10 km s-1. High Alfvén speeds may well occur within active regions, such as already found for HH 34, where the results of multiple outflow events are being observed. Origins for the low but significant level of pre-shock ionization, a prerequisite for a jump shock, are considered.
The excitation state of H2 in local thermodynamic equilibrium is calculated. For planar shocks, extremely low (but non-zero) H2O fractions are indeed necessary to match the observed OMC-1 column densities. However, gas-grain cooling then dominates and the planar model is still inadequate. Bow-shock models overcome these problems. A fast bow shock possesses an oblique tail region where the normal flow speed is below the molecular dissociation limit and warm H2 survives. A paraboloidal bow in gas of density 10 then allows an H2O abundance of 3 × 10-6 for OMC-1. Bows with longer tails reproduce the H2 data with an arguably acceptable H2O abundance of 3 × 10-5.
The planar and bow models result in overproduction of CO rotational emission unless CO abundances less than 10-5 are admitted. Even then, a secondary source must still be invoked to explain the CO line ratios. The degree of excitation of the H2O molecule provides a means of distinguishing shock structures and shock physics. The H2O excitation differences are estimated here, and are measurable by the Infrared Space Observatory. Differences in linewidths between types of jump and continuous shocks are also predicted.

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