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Model development of supersonic trough wind with shocksThe time dependent one dimensional hydrodynamic equations describe the evolution of the thermal plasma flow along closed magnetic field lines outside of the plasmasphere. The convection of the supersonic polar wind onto a closed fieldline results in the assumed formation of collisionless plasma shocks. These shocks move earthward as the field line with its frozen-in plasma remains fixed or contracts with time to smaller L coordinates. The high equatorial plasma temperature (of the order of electron volts) produced by the shock process decreases with time if the flow is isothermal but it will increase if the contraction is under adiabatic conditions. Assuming adiabaticity a peak in the temperature forms at the equator in conjunction with a depression in the ion density. After an initial contraction, if the flux tube drifts to higher L coordinates the direction of the shock motion can be reversed so that the supersonic region will expand along the field line towards the state characterizing the supersonic polar wind. A rapid expansion will lower the equatorial density while the temperature decreases with time under adiabatic but not isothermal conditions.
Document ID
19720011673
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Grebowsky, J. M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
September 2, 2013
Publication Date
February 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
X-621-72-53
NASA-TM-X-65848
Report Number: X-621-72-53
Report Number: NASA-TM-X-65848
Accession Number
72N19323
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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