Results 1 to 10 of about 7,427 (211)

Experimental Study of the Combustion Efficiency in Multi-Element Gas-Centered Swirl Coaxial Injectors

open access: yesEnergies, 2020
The effects of the momentum-flux ratio of propellant upon the combustion efficiency of a gas-centered-swirl-coaxial (GCSC) injector used in the combustion chamber of a full-scale 9-tonf staged-combustion-cycle engine were studied experimentally.
Seongphil Woo   +3 more
doaj   +3 more sources

Vortex Breakdown Control by the Plasma Swirl Injector [PDF]

open access: yesApplied Sciences, 2021
Vortex breakdown, observed in swirling flows, is an interesting physical phenomenon relevant to a wide range of engineering applications, including aerodynamics and combustion.
Gang Li   +6 more
doaj   +3 more sources

Spray Pattern Investigation using Swirl Injector for Liquid Rocket Engine

open access: yesChemical Engineering Transactions, 2018
This paper aims to represent the experimental investigation of spray pattern in swirl injector. For this purpose, an experimental setup is fabricated and spray pattern investigation is carried out.
B. Ravi Kumar, V. Srihari
doaj   +2 more sources

Design and Analysis of Pressure- Swirl Fuel Injector with Full- Cone Spray for Catalytic Thruster [PDF]

open access: yesعلوم، فناوری و کاربردهای فضایی, 2022
The monopropellant thrusters of the situation control system are a requirement for the development and application of satellites and space capsules in space, which are high-tech and expensive. In this paper, the design and simulation of a pressure- swirl
Hadiseh Karimaei
doaj   +1 more source

Investigation of Effect of Rheological Behavior of Gelled Propellant on Atomization Characteristics of Swirl Injector [PDF]

open access: yesفناوری در مهندسی هوافضا, 2021
The Gelled propellants have a promising future for aerospace applications because of possessing the advantages of both solid and liquid propellants. A gel propellant is a liquid propellant whose rheological properties have changed by the addition of ...
Ali Saberi moghaddam   +2 more
doaj   +1 more source

Experimental Study of Spray Merge in Dual Pressure- Swirl Coaxial Injectors [PDF]

open access: yesعلوم، فناوری و کاربردهای فضایی, 2022
The purpose of this paper is to present experimental data for merging two outlet fluid skirts in a dual pressure- swirl coaxial injector. In this study, a dual pressure- swirl external mixing injector was designed and fabricated.
ALI RASTGAR, Hojat Ghasemi
doaj   +1 more source

Design and Simulation of Single Capillary Injector and Circular Injector Plate for a Monopropellant Thruster [PDF]

open access: yesفصلنامه علوم و فناوری فضایی, 2022
In this research, design and simulation of a single capillary injector and three-hole circular injector plate of a 10N Hydrazine monopropellant thruster were performed. Ansys Fluent software was used to simulate the injector and injector plate .
Sajad Davari, Hadiseh Karimaei
doaj   +1 more source

Numerical Study on Combustion and Atomization Characteristics of Coaxial Injectors for LOX/Methane Engine

open access: yesInternational Journal of Aerospace Engineering, 2021
The LOX/methane engine has an admirable performance under a supercritical state. However, the properties of methane change drastically with varying injection temperature.
Jiabao Xu   +4 more
doaj   +1 more source

Analyzing Combustion Efficiency According to Spray Characteristics of Gas-Centered Swirl-Coaxial Injector

open access: yesAerospace, 2023
The momentum flux ratio (MFR) significantly affects the mixing characteristics and combustion efficiency of propellants in rocket engine injectors. The spray characteristics of three gas-centered swirl-coaxial injectors used in a full-scale combustion ...
Seongphil Woo   +5 more
doaj   +1 more source

Swirled injector modeling for cavitating multiphase flow [PDF]

open access: yesE3S Web of Conferences, 2019
The goal of this study is to present a comparison between different approaches to multiphase injection modeling of self-pressurized rocket engine propellant. Swirled, tangential orifice injector of nitrous oxide, for an “N” class hybrid rocket motor is the object of the study.
Ziegler Bartosz   +2 more
openaire   +2 more sources

Home - About - Disclaimer - Privacy