Aircraft Engineering
Аuthors
Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia
e-mail: nikitchenko7@yandex.ru
Abstract
A problem is considered for a flow past an infinitely thin plate installed at a zero angle of attack in a hypersonic flow. The NSF model is accepted as a physico-mathematical flow model. Calculations are made with the use of McCormack explicit scheme and Thomas algorithm. Two methods of boundary conditions setting on a solid surface are considered. It is shown that in the strongly non-equilibrium flow region application of the NSF model results in qualitatively incorrect results when calculating normal voltages.Keywords:
hypersonic flow, thin plate, Navier-Stokes model, boundary conditions.
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