
On the efficiency of using the Navier-Stokes approximation in thermogasdynamic calculation of low-thrust liquid-propellant rocket engines at low Reynolds numbers
Author(s) -
A. D. Maksimov,
С. А. Шустов
Publication year - 2022
Publication title -
vestnik samarskogo universiteta. aèrokosmičeskaâ tehnika, tehnologii i mašinostroenie
Language(s) - English
Resource type - Journals
eISSN - 2541-7533
pISSN - 2542-0453
DOI - 10.18287/2541-7533-2022-21-1-67-80
Subject(s) - thrust , aerospace engineering , liquid propellant rocket , reynolds number , propellant , rocket (weapon) , spacecraft , mechanics , software , flow (mathematics) , computational fluid dynamics , propulsion , physics , computer science , engineering , turbulence , programming language