• Proceedings of the Korean Society of Propulsion Engineers Conference
• /
• 2011.04a
• /
• pp.132-135
• /
• 2011

A technology for buzz margin determination is suggested to obtain stable shock structure and high compression efficiency of supersonic intake. By using the shock equilibrium equation of supersonic intake, sensitivity equation of terminal shock position for free stream and back pressure is induced and disturbances are quantified through statistical approach. Numerical results show that the sensitivity of shock position for disturbances is proportional to Mach number and the back pressure is dominant for variance of terminal shock position.

• Journal of the Korean Recycled Construction Resources Institute
• /
• v.9 no.1
• /
• pp.85-91
• /
• 2021

Aggregate waste separator with rotating separating net was designed for applying classification process of construction waste. In order to evaluate the performance of the aggregate waste separator, according to the type of waste, standardized waste samples are prepared using acrylic. The appropriate operating point was evaluated by the classification efficiency and misclassification rate of recycled aggregate according to the control frequency of the blower operating and inlet position of the separating net. The classification efficiency at the operating point of the aggregate waste separator was evaluated through flow analysis assuming recycled aggregate and waste sample as particles. As a result of the performance test, when the distance. between the conveyor belt and the inlet was 0.2m, the classification efficiency was 95%, but the misclassification rate of recycled aggregate was 2% or more, which satisfies the classification efficiency and the misclassification rate of less than 2%. The operating point was shown at a control frequency of 58Hz at a suction distance of 0.254m. As a resu lt of flow analysis, there was no misclassification of recycled aggregate. In order to redu ce constru ction waste in the existing recycled aggregate production process, adsorption system using a rotating separating net that can be operated as an installation type was built.

• The Journal of the Acoustical Society of Korea
• /
• v.12 no.6
• /
• pp.28-35
• /
• 1993

팬소음은 설계변수들과 관계가 있으므로 본 논문은 실험적 방버벵 의하여 팬소음과 설계변수의 관계를 고찰하였다. 설계변수는 팬소음에 특히 영향이 큰 날개수, 날개각도, 날개끝 간극을 선택하였으며 새로운 설계변수로서 동익과 정익간의 간극과 흡입구 길이를 고찰하였다. 본 논문은 팬소음에 대한 관련된 이론을 정리하였으며 축류형 팬의 고효율 저소음 설계를 위한 방안을 제시하였다. 흡입구 길이, 날개끝 간극, 동익과 정익간의 간극등의 설계변소를 변경하여 실험한 결과 이들 설계변수들의 조정에 m이하여 축류형 팬의 고효율 저소음화를 이룰 수 있었다.

• Journal of the Korea Academia-Industrial cooperation Society
• /
• v.18 no.2
• /
• pp.31-37
• /
• 2017

This paper investigates the effect of the rotational motion of a driving fluid generated by a rotational motion device at the inlet of a driving nozzle for a gas-liquid ejector, which is the main device used for ozonated ship ballast water treatment. An experimental apparatus was constructed to study the pressure and suction flow rate of each port of the ejector according to the back pressure. Experimental data were acquired for the ejector without rotational motion. Based on the data, a finite element model was then developed. The rotational motion of the driving fluid could improve the suction efficiency of the ejector based on the CFD model. Based on the CFD results, structure optimization was performed for the internal shape of the rotation induction device to increase the suction flow rate of the ejector, which was performed using the kriging technique and a metamodel. The optimized rotation induction device improved the ejector efficiency by about 3% compared to an ejector without rotational motion of the driving fluid.

• Journal of the Korean GEO-environmental Society
• /
• v.10 no.5
• /
• pp.5-9
• /
• 2009

In this experiment, the cutter head was designed as the down-scaled shape from the cutter head of the Asan-3 of Hyundai Construction Company. The dredging simulation instrument was installed in the experiment water tank which has the dimension of $4.2m(L){\times}2.2m(W){\times}1.5m(H)$. The speed of all components were controlled manually through the hydraulic tool and motors to find the effective desilting condition. As the results, the experiment was conducted to find the optimate dredging cutter head operation rate. To compare the factors which effect on the dredging effectiveness, the dimensionless dredging volume ratio was introduced and it can be found the best effectiveness at 2.0 m/s suction speed, 8 cm dredging depth and 4~4.5 dimensionless dredging volume ratio. Therefore, in order to take the best effectiveness these 3 components factors should be adequately considered.

• Journal of the Korea Organic Resources Recycling Association
• /
• v.21 no.3
• /
• pp.74-81
• /
• 2013

In this study, the separation efficiency of wind power selector (the direction of the air flow of the air to perform gravity separation method) of municipal solid waste which was landfilled was investigated to reduce amount of waste that is designed to increase the recycling rate of wastes for the ANSYS CFX Program's numerical methods with wind through the separator. When a suction device designed to suction 1000mL of a plastic bag, the separation efficiency was 100% and when the wind speed was 0.9 m /sec or more and when the wind speed was 1.6 m / sec or more, the efficiency of plastic bottles in a mixture of 500mL and 1500mL plastic bottle waste was 100% and the aluminum screening efficiency of 250mL aluminum can was 100 % when the wind speed was 2.3 m / sec. In the last, 5mm thick compressed aluminum can efficiency was 90 % when the wind speed was 2.4 m / sec.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.6 no.2
• /
• pp.65-74
• /
• 2002

Optimal supersonic diffuser shape of integrated rocket ramjet engine was derived which maximizes the total pressure recovery. Mass flux is considered as a design constraint and the second oblique shock angle of the external ramp, the cowl-lip angle and the throat area are selected as design variables. Refined response surface method through design space transformation technique was developed and employed, and high confidence level of the regression model could be obtained. Genetic algorithm was implemented for both system optimizer and subspace regression model optimization. Virtual nozzle was located at the end of throat to adjust the back pressure. With only 20 aerodynamic analyses, optimal supersonic diffuser shape which has 14% improved total pressure recovery characteristics was successfully designed.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.20 no.4
• /
• pp.104-111
• /
• 2016

The flame stabilization is one of the topics which have to be solved for the airbreathing propulsion systems, using the entering air which is supersonic velocity as an oxygen sources. Making a recirculation zone with an eddy flow, installed the reducing velocity devices such as the bluff body, is the typical method of the flame stabilization. Recently using a cavity flame stabilization at the wall is an emerging technique as an effective method which extends the stabilization zone, and the related research papers have been published on the flow separation and reattachment, pressures and oscillations including length/depth ratios in the cavities. Even though, still there are lots of topics to study more in the cavity flame stabilization field as the preceding techniques, as well as the research and the development of the airbreathing propulsion system itself.

• Transactions of the Korean Society of Mechanical Engineers B
• /
• v.38 no.12
• /
• pp.1065-1072
• /
• 2014

The shape of an impeller splitter for a dual-inlet centrifugal blower was optimized to enhance the blower performance. Two design variable, the normalized chord and pitch of a splitter, were used to evaluate the blower performance and internal flow fields based on the three-dimensional flow analysis. The blower performance obtained using this numerical simulation had a maximum error of 4 percent compared to that in an experiment at the design flow condition. The shape optimization of the splitter successfully increased the blower efficiency and pressure by 3.65 and 1.14 percent compared to the reference values. The blower performance was increased by reducing the flow separation near the blade suction surface by optimizing the shape of the splitter, which produced a pressure increase at the outlet of the volute casing.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
• /
• 2014.04a
• /
• pp.244-245
• /
• 2014