Results 111 to 120 of about 16,009 (301)

Mathematical simulation of choking under self-oscillations in hydraulic systems with cavitating pumps of liquid-propellant rocket engines [PDF]

, 2020
S.I. Dolgopolov
openalex   +1 more source

Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions [PDF]

Ablative response of silica phenolic to simulated liquid propellant rocket engine operating ...
Moyer, C. B., Powars, C. A., Rindal, R. A., Wool, M. R.   +3 more
core   +1 more source

Erratum to: “Numerical and experimental investigations of the effect of repeated cyclic thermal loads on the strength of materials of recoverable liquid-propellant rocket engines” [PDF]

, 2009
V. I. Bubnov, D. V. Isakov, I. G. Lozino-Lozinskaya, A. M. Polyanskiǐ   +3 more
openalex   +1 more source

Rocket motion [PDF]

arXiv
The motion of rockets is part of the study devoted to the motion of variable mass systems. Notably those in which the mass leaves permanently the considered system. Rockets are propelled forward by the reaction force produced by the hot exhausted gases ejected from their tales in the rearward direction.
arxiv  

Simulation Study on Outflow Characteristics of Cryogenic Propellant during Rocket Ascent

Zhileng xuebao, 2020
At the rocket launching stage, it is very important to supply sufficient and vapor-free liquid propellant to maintain the functioning of the main engine.
Huang Xiaoning, Wang Lei, Mao Hongwei, Xue Liangjiang, Li Yanzhong   +4 more
doaj  

EMF Frequency Response Investigation of Liquid-Propellant Rocket Supersonic Jet [PDF]

, 2012
Д.А. Ягодников, А.В. Рудинский   +1 more
openalex   +1 more source

Nonlinear combustion instability in liquid-propellant rocket motors Final report [PDF]

Mathematical models of nonlinear combustion instabilities in liquid propellant rocket ...
Burstein, S. Z., Chinitz, W., Schechter, H. S.   +2 more
core   +1 more source

The problem of combustion instability in liquid rocket engines

Challenges and Issues of Modern Science
The purpose of this work is to carry out an overview on combustion instability in liquid propellant rocket engines, its classification, the main principles of occurrence as well as ways to prevent the phenomena while designing of the prospective engine.
Samir Vekilov, Volodymyr Lipovskyi, Roman Pustovyi   +2 more
doaj  

Application of the substructure method for thermal stress-strain assessment of a liquid-propellant rocket engine combustion chamber [PDF]

, 2013
С.С. Гаврюшин, Е.Е. Красновский, О.В. Короткая, Павел Петрович Стриженко, Р.Э. Катков   +4 more
openalex   +1 more source

Theoretical investigation on transverse mode combustion instability for liquid propellant rockets [PDF]

Mathematical solution of nonlinear transverse combustion instability problems in thin annular liquid propellant rocket ...
Crocco, L., Lorenzetto, J. H.
core   +1 more source