Unsteady Flow and Pressure Pulsations in a ModelAxial-Vortex Stage Inducer
1.
Rocket Engines Department,Moscow Aviation Institute（National Research University）,Moscow 125993,Russia;2.
School of Astronautics，Beihang University,Beijing 100083,China
发布日期:2021-08-15
作者简介:Sergey Timushev，PhD，professor, in research of simulation and test of turbo-pumps. E-mail：irico.harmony@gmail.com
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