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
Dependencies for velocity slipping and temperature jump within the broad range of Knudsen numbers are proposed. Phenomenological approach is used for forming molecule distribution function in the boundary point.Keywords:
boundary conditions, solid surface, distribution function.
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