Numerical method for calculating the nozzle thrust of a wide-range rocket engine

Numerical method for calculating the nozzle thrust of a wide-range rocket engine

A numerical method for calculating the thrust of a wide-range rocket engine nozzle has been developed. This type of engine is equipped with an annular nozzle with a flat central body and is designed to operate in the upper atmosphere and in vacuum. The nozzle forms a jet converging to the axis of sy...

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Bibliographic Details
Main Authors: Alyona A. Kirshina, Artyom A. Levikhin, Anton Yu. Kirshin
Format: Article
Language:English
Published: Saint Petersburg National Research University of Information Technologies, Mechanics and Optics (ITMO University) 2022-10-01
Series:Naučno-tehničeskij Vestnik Informacionnyh Tehnologij, Mehaniki i Optiki
Subjects:
wide-range rocket engine
thrust
nozzle
numerical simulation
Online Access:https://ntv.ifmo.ru/file/article/21534.pdf

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