• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.10
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• pp.60-65
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• 2003

An experimental study was performed to understand ignition characteristics of gas turbine combustor with rotating fuel injection system. Liquid fuel applied to the inner surface of rotating fuel nozzle which was driven by high speed electrical motor is flung away by centrifugal forces. The real scale combustor and test rig was manufactured and tested under atmospheric condition in KARl combustion test facility. From the test results, this combustor ignition characteristics are highly dependent upon fuel nozzle rotating speed. Futhermore, combustor exit gas temperature was rapidly changed by increasing or decreasing the fuel nozzle rotating speed.

• Proceedings of the Materials Research Society of Korea Conference
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• 2011.05a
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• pp.41.1-41.1
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• 2011

초소수성 표면은 $150^{\circ}$ 이상의 높은 접촉각을 가지며 표면에 오염물질이 묻지 않게 하는 anti-contamination, anti-fingerprint, self-cleaning 기능을 갖고 있는 것이 특징이다. 재료표면의 친/소수성을 제어하기 위해서는 고체 표면의 화학적인 요인과 물리적인 요인 두 가지를 조절함으로써 이루어지는데 즉 물질의 표면에너지와 표면 거칠기를 변화시켜 친/소수성을 부여할 수 있다. 초소수성 표면을 구현하기 위해서는 고체 표면의 에너지를 낮춰야 하며 이는 일반적으로 불소화합물을 사용한다. 불소는 지구상의 원소 중 가장 낮은 표면에너지를 가지고 있어 주로 후라이팬이나 치아 표면에 코팅되며 오염을 방지하는 특성을 지닌다. 실리카는 박막소재로 이용하기 위한 우수한 특성을 가진 물질로서 자연계에서 매우 풍부하게 존재하고 있으며, 생체무해하며 내구성과 내마모성, 화학적 안정성, 고온 안정성 등을 지니고 있어 여러 가지 종류의 전자기기 및 부품의 내외장 코팅에 적용이 적극 검토되고 있다. 이러한 실리카 코팅소재를 바탕으로 초소수성 코팅층을 구현하는 하나의 방법으로서 본 연구에서는 전기분무법을 사용하여 실리카 코팅층을 형성하였으며, 표면에너지를 제어하기 위해 플루오린 처리를 하여 초소수성 실리카 코팅층을 제조하였다. 합성된 실리카 코팅층은 물 뿐만이 아니라 표면장력이 낮은 다른 용액에서도 초소유성을 나타내었다. 이러한 코팅층에 대한 고온 안정성과 UV 저항성, 내구성(durability) 등을 조사하여 실제 응용 가능성을 타진하였다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.04a
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• pp.168-171
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• 2007

A technical review of current slurry and gelled propellants is presented. In advanced countries, it is confirmed that these propellants have high specific impulse, density, excellent handling, safety characteristics and thrust controllability through research since 1950s. Substantial researches have been pursued to characterize the rheological properties, spray/combustion phenomena and propulsion system design for the gel propellant characteristics. Slurry and gelled propellants are developing actively to applicate both military and space propulsion fields such as tactical missile, air-breathing ramjet, pulse detonation engine, and combined cycle engine of future propulsion mode.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.1016-1020
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• 2017

This study was conducted to develop a test facility that simulates the combustion instability that occurs in a real-scale liquid rocket combustor. A separate engine head with 3 injectors arranged in a row was designed/manufactured and verified through preliminary tests. The flow rate and spray pattern of the head were confirmed by the cold flow test. Next, propellant spray test and combustion test were carried out. A preliminary combustion test was carried out at 10 bar and the combustion chamber pressure was measured to be significantly lower than the target pressure. This is because it was a low pressure test, and it is expected to be resolved in the high pressure test in the future.

• Journal of the Korean Crystal Growth and Crystal Technology
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• v.16 no.6
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• pp.244-249
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• 2006

Electrostatic spray pyrolysis, a novel fabrication technique, has been used in this study to prepare calcium phosphate nano powders. Final annealing was done at $400^{\circ}C$ for 30min in air. The hydroxyapatite - forming ability of the annealed powder has been evaluated in Eagle's minimum essential medium solution (MEM). X-ray diffraction analysis, field emission - scanning electron microscope, energy dispersive X-ray spectroscope, and Fourier transform infrared spectroscope were used to characterized the annealed powders after immersion in MEM. The powder with an amorphous structure induced hydroxyapatite formation on their surfaces after immersion fer 15 days.

• Korean Journal of Agricultural Science
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• v.6 no.2
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• pp.192-197
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• 1979

Spread factors were tried to determine the diameter of airborne droplet emitted: from the sprayer by the measurements of airborne droplet diameter emitted from the uniform size droplet producer and impression diameter on Kromekote card or Eucalypt's leaf in the different dilute concentration with Geigy Red Herbicide Dye from 0.5% to 2% by weight. The results abtained were as follows; The general form of the equation in the relationship between airborne droplet and impression diameter on Kromekote card or Eucalypt's leaf was an exponential equation as follows; $$Y=aX^b$$ which gave a linear relation on log-log graph paper. The spread factor seemed to be larger in the thin dilute concentration than in the thick dilute concentration. The spread factor was remarkably smaller on Eucalypt's leaf than on Kromekote card due to the penetration of liquid into the leaf and the stomata of the epidermis. The calculated equation of the mean depth of the droplet sprayed on Eucalypt's leaf was the same form as $Y=aX^b$, which implied that the spray liquid was distributed in surplus in accordance with the diameter of the droplet larger than the optimum size droplet to control insect and disease.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.30 no.5
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• pp.79-87
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• 2002

Acoustic responses to pressure oscillations in axisymmetric combustion chamber are numerically investigated to examine the qualitative trend of acoustic instability in liquid rocket engine. Chamber operating condition and excitation frequency of oscillating pressure are selected as exciting parameters of acoustic instability. Artificial perturbation is simulated by total-pressure oscillation with sine wave at chamber inlet. Many approximations and simplifications are introduced without losing the essence of acoustic pressure response. First, steady-state solution for each operating condition is obtained and next, transient analysis is conducted. Depending on operating condition and excitation frequency, the distinct response characteristics are brought. Weak-strength flames and high-frequency excitation tend to cause sensitive acoustic pressure response leading to unstable pressure field. These results are analyzed based on the correlation with acoustic pressure responses from the previous works adopting laminar flamelet model.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2009.05a
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• pp.277-280
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• 2009

Mechanism of combustion frequencies occurring during combustion is experimentally investigated in model combustor with V-gutter flameholder. this combustor has a long duct shape with a cross section area of $40{\times}40\;mm$. The v-gutter type flameholder with 14mm width is mounted at the bottom of combustor. Kerosene and methane were used as fuel, and these fuel were injected transversely into air crossflow. It is found that combustion frequencies were considered as 1L longitudinal mode caused by combustor geometry and vortex shedding mode of flameholder. And fuel phase effect and nozzle effect were also observed in the low frequency range.

• Proceedings of the KAIS Fall Conference
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• 2011.12b
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• pp.540-542
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• 2011

본 논문은 결로 방지 기능을 가진 배전반 개발을 위해 다양한 온습도 환경 조건에서 결로의 생성 및 제거에 관한 특성을 파악하였다. 획득된 결과는 외부 온도변화에 따라 배전반 내부의 온도도 변화되며, 내외부의 온도차는 일정한 차이를 나타내었다. 결로 생성의 특성은 초기에는 미세한 분무상에서 시간이 경과함에 따라 주위 물방울들과 결합하여 성장하며, 최종적으로는 표면장력이 작용하지만 중력에 의해 하부로 처지면서 떨어지는 과정으로 진행되었다. 또한 히터 등으로 결로 생성조건을 파괴시키면 생성시와 동일한 온습도 조건이 유지되어도 결로는 제거되는 것을 알 수 있었다.

• Journal of the Korean Society of Safety
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• v.19 no.3 s.67
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• pp.20-25
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• 2004

In order to obtain the flame Propagation speed in freely falling droplet suspension Produced by an ultrasonic atomizer, a light collecting probe named Multi-color Integrated Cassegrain Receiving Optics (MICRO) is applied to spark-ignited spherical spray flames. Two MICRO probes are used to monitor time-series signals of OH chemilumine-scence from two different locations in the flame. The flame propagation speed is calculated by detecting the arrival time difference of the propagating flame front. In addition, time-series images of OH chemiluminescence are simultaneously obtained by a high-speed digital CCD camera to ensure the validity of the MICRO system. Furthermore, relationship between the spray properties measured by phase Doppler anemometer (PDA) and the flame propagation speed are discussed with k different experimental conditions by changing the fuel injection rate. It was confirmed that the MICRO probe system was very useful and convenient to obtain the flame propagation speed and that the flame propagation speed was different depending on the spray properties.