NASA NTRS · 20060032262
Modeling Non-Axisymmetric Bow Shocks: Solution Method and Exact Analytic Solutions
Abstract
A new solution method is presented for steady-state, momentum-conserving, non-axisymmetric bow shocks and colliding winds in the thin-shell limit.
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Wilkin, F.. 2000-01-01. Modeling Non-Axisymmetric Bow Shocks: Solution Method and Exact Analytic Solutions. https://ntrs.nasa.gov/citations/20060032262
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