• Journal of the Korean Society of Propulsion Engineers
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• v.16 no.5
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• pp.1-9
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• 2012

The gas jet from a coaxial porous injector for two-phase flows is discharged from the porous surface, which encloses the center liquid jet, and the gas and liquid jet interact with each other physically. The wall injected gas jet transfers the radial momentum effectively while the radial gas jet develops to axial jet, and the performance of atomizing and mixing can be improved. In this study, the Weber number and the ratio of momentum flux were controlled by changing the gas injection area and the mass flow rate of the gas jet, and a study on the spray characteristics at the cold-flow test using water and air simulant was performed. It is concluded that the radial momentum transfer concept of a coaxial porous injector gives a positive effect on the atomization and mixing of the two-phase spray.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.6-6
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• 1998

항공기용 가스터빈 및 일반적인 산업용 분무시스템에서는 많은 양의 분사액체를 미립화 시키고 시스템의 연속적인 운전과 유지를 편리하게 하기 위하여 여러 개의 분사노즐을 열로 설치하여 동시에 분사하도록 하고 있다. 이렇게 동시에 분사할 경우, 노즐간에 거리가 충분히 크지 않으면 개별적으로 분사된 분무들이 서로 합해져서 하나의 연합된 분무군이 형성된다. 이렇게 Two element에 의해서 형성된 spray는 공급압력이 증가함에 따라 관성력이 증가하게 되어 중심부분에서 액막 혹은 액적상태로서 충돌이 발생하여 복잡한 분무특성을 가질 것이다. 따라서, 연합된 분무군의 특성을 이해하는 것은 응용의 측면에서 매우 중요하다고 할 수 있다.

• Journal of the Korean Society of Propulsion Engineers
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• v.9 no.3
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• pp.92-100
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• 2005

An optimal fuel manifold is suggested to improve the cooling performance of an injector face plate. The cooling performance at the center area of the injector face plate is to be augmented while the spatial injection uniformity is maintained. The comparison of the cooling performance of f candidates gives the conclusion that the dividing plate from 2-3 injector .ow to 9-10 injector. row is an optimal. The maximum face plate temperature decreases by 27$\%$ while the injection uniformity is close to that of the original design. The pressure drop in the fuel manifold of the optimal design is also same as the original design.

• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.2
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• pp.39-45
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• 2016

In a coaxial porous injector, a gas propellant is injected through the porous cylinder surface to the liquid jet which is encircled by a porous cylinder. In this study, to observe the differences in disintegration mechanisms between a shear coaxial injector and a coaxial porous injector, cold-flow tests and 2-D axisymmetric numerical analysis have been carried out. The shadowgraph images and Sauter mean diameters were compared in similar experimental conditions, and the effects of velocity distributions at the inner injector region on the disintegration of liquid jet were investigated through the numerical calculations. As a result, in high air mass flow rate condition, the disintegration performance of coaxial porous injector is better than shear coaxial injector, in spite of a lower velocity at the inner injector region.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.215-218
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• 2005

An optimal fuel manifold is suggested to improve the cooling performance of injector face plate. The cooling performance at the center area of the injector face plate is to be augmented while the spatial injection uniformity is maintained. The comparison of the cooling performance of 7 candidates gives the conclusion that the dividing plate from 2-3 injector row to 9-10 injector row is an optimal. The maximum face plate temperature decreases by $27\%$ while the injection uniformity is close to that of the original design. The pressure drop in the fuel manifold of the optimal design is also same as the original design.

• Aerospace Engineering and Technology
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• v.1 no.2
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• pp.113-122
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• 2002

A numerical analysis on the uniformity of propellant injection velocity of KSR-III has been carried out to give design improvements. Injector holes were approximated as porous media with the same pressure drop . The injection velocity is higher at the opposite side of the inlet for both LOX and fuel due to the static pressure rise in the stagnation region. Flow passages at the vertical circular plate in the LOX dome increase the uniformity of LOX injection. Little change was observed in the injection uniformity and pressure drop for the slanted LOX passage. Also provided were the O/ F ratio distributions from the oxidizer/ fuel injection velocity analysis.

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.6
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• pp.126-142
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• 2020

This study aims to provide basic design data for a pintle injector and its combustion device through case study on the research and development of combustion devices to which a liquid-liquid pintle injector was applied. From data analysis, it was possible to provide the initial dimension of the combustion chamber and pintle injector based on the engine thrust, and the geometric characteristics of the high-efficiency injector. In addition, the pintle tip heat damage prevention mechanism and materials, face-shutoff pintle injector implementation method, and central propellant selection criteria were summarized. Theses results will be used as basic data for the design criteria of an initial pintle injector combustion device.

• Transactions of the Korean Society of Automotive Engineers
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• v.5 no.2
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• pp.80-86
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• 1997

This experiment was undertaken to investigate spray characteristics of the conventional injection system and the ultrasonic energy added injection system. Sauter mean diameter was measured under the variation of injection pressure and the spray distance. To measure the droplet size, we used the Malvern system 2600C. The spray angle and mass distribution were analyzed to the CCD camera and the patternater. After experiment, it was found that the ultrasonic energy added injection system had smaller Sauter mean diameter of droplet, wider mass distribution and wider spray angle than the conventional injection system had.

• Journal of the korean Society of Automotive Engineers
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• v.3 no.1
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• pp.5-12
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• 1981

최근 세계의 자동차업계에 문제가 되고 있는 연료경제 및 배기공해와 더불어 출력향상을 위하여 채택되고 있는 가솔린 기관의 연료분사장치는 유럽을 중심으로 하여 미국 및 일본에서 급속하게 발전되고 있으며 상당한 수의 자동차가 이를 장착, 주행하고 있어 향후 이러한 추세는 더욱 늘어날 전망에 있으므로 우선 이에 대한 개요를 소개함으로써 국산자동차의 기술적 향상에 기여 코자 한다.

• Journal of the Korean Society for Marine Environment & Energy
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• v.10 no.2
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• pp.118-124
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• 2007

The oceans could absorb almost all the anthropogenic carbon dioxide the mankind has been producing eventually, but in the nature the air-sea $CO_2$ exchange occurs very slowly and to lower the atmospheric $CO_2$ concentration substantially $CO_2$ must be injected to the interior of the ocean directly. If we inject $CO_2$ collected at the major $CO_2$ sources into the international waters in the Philippine Sea or east of Japan, we could store the $CO_2$ in the oceans effectively for a few hundred years. When $CO_2$ is dissolved into the water, PH drops. The creatures adapted to the deep oceans where environment is very stable could be affected by even a small change in pH significantly. If, therefore, we are to inject $CO_2$ into the oceans, we must assess the effect of $CO_2$ injection in the marine ecosystem beforehand. Only when the damage to the marine ecosystem is smaller than the benefit from the $CO_2$ injection, $CO_2$ injection is effective.