The Hysteresis of Propeller Ejection Transition for Gravimetric Rotator Model

Details The Hysteresis of Propeller Ejection Transition for Gravimetric Rotator Model The Hysteresis of Propeller Ejection Transition for Gravimetric Rotator Model

Jul 1987

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1987atsir1502....1p&link_type=abstract

Astronomicheskii Tsirkulyar NO.1502/JUL, P. 1, 1987

Astronomy and Astrophysics

Astronomy

1

Scientific paper

An asymmetry of a magnetic neutron star transition from ejecting to
propeller state by non-stationary accretion is investigated. The
critical orbital eccentricity is found for the hysteresis to occur.

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