• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1992.10a
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• pp.31-35
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• 1992

자동차 관련 소음 및 진동중 엔진과 관련된 것은 흡.배기계 소음과 엔진 자 체의 각 구동 부위 및 연소실 소음으로 대별하여 볼수 있다. 특히 연소실 소 음의 경우에는 엔진 내부에서 발생하는 진동과 압력파가 엔진을 진동시키고, 이러한 엔진의 진동이 방사음을 발생시켜 형성되는 만큼 그 해석 및 공학적 접근 방법이 용이하지 않다. 연소실 소음은 압력의 갑작스런 변화에 의한 폭 발소음과 피스톤과 실린더 벽면의 충돌에 의한 피스톤 슬랩(piston slap)으로 크게 구분할 수 있으며 압력이 높지 않고 압력의 변화가 빠르지 않을 경우 에는 피스톤 슬랩이 기계적 소음의 주 원인이 되는 것으로 알려져 있다. 본 고에서는 피스톤 슬랩에 의한 진동 현상을 예측하기 위한 이론적 접근 방법 을 제시하고 이의 타당성을 검증하기 위한 실험적 방법을 제시하고자 한다. 또한, 피스톤과 실린더의 간극 진단을 위해 슬랩 신호를 이용하는 방법에 대 해 살펴보고, 피스톤과 실린더의 충돌 속도를 통해 슬랩 신호를 줄이기 위한 엔진의 설계 방법에 대해 살펴보고자 한다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2010.05a
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• pp.173-174
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• 2010

• The Journal of the Acoustical Society of Korea
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• v.37 no.4
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• pp.242-247
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• 2018

The automotive industry is making various efforts to cope with ever-increasing exhaust emissions and fuel economy regulations. However, this often results in degraded NVH (Noise, Vibration, and Harshness) performance. For example, we proposed the causes and improvements for the noise generated by the high-pressure pump noise of a gasoline engine, the change of acceleration noise due to dual injection of MPI (Multi-Point Injection) and GDI (Gasoline Direct Injection), the noise of a gasoline turbocharger, and the combustion noise deteriorated due to the injection parameters calibration in a diesel engine. Since these noises are caused by the high frequency noise, and the driver feels the rough sound quality, efforts to reduce them with proper NVH measures are indispensable.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1998.05a
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• pp.87-94
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• 1998

폭발현상(explosion phenomena)이 항상 연소(combustion)를 수반하는 것도 아니고, 연소현상이 항상 폭발적으로 일어나는 것이 아님에도 불구하고 많은 사람들은 폭발과 연소 사이에 밀접한 관계가 있는 것으로 생각하고 있다. 일반적으로 폭발이라고 하면 우선 큰 소리와 건물이나 실내의 파괴를 연상한다. 폭발 시에 발생하는 큰소리, 이른바 폭발음은 공기 중을 전파하는 압력파(blast wave)에 의한 것이고 건물이나 실내 파괴는 그들의 내부압력 상승에 의한 것이다. 그러므로 폭발현상은 압력상승과 불가분하다고 생각해도 된다. (중략)

• 전기의세계
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• v.44 no.10
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• pp.23-27
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• 1995

가전기기의 진동과 소음은 제품의 고품질화에 상당히 저해되고 진동에 의한 소음이나 소음에 의한 진동을 해석하기 위하여 부단하게 노력하고 있다. 소리를 음이라 하며 음의 발생을 매질의 움직임에 의한 에너지 전달로 이해하고 있다. 따라서 음은 파동을 가지게 되어 음파(sound wave)로 불리우는 파에 의해 이동되며 이동시 주위의 매질에 압력 파동을 유발시킨다. 따라서 실내에서 발생하는 소리와 목욕탕등에서 나는 소리는 매질의 다른 성질(공기밀도)에 의해 다르게 느껴진다. 일반적으로 음의 주파수라하면 1초동안 음의 고저가 몇번 발생하였는가를 의미하며 사람이 소리로서 느끼는 주파수 범위를 20Hz에서 20kHz로 나타내어 가청 주파수라 한다. 그러나, 소리중에서도 사람에게 불쾌감을 일으키거나 심하면 고통까지 유발시키는 원하지 않는 소리가 있는데 이를 소음(noise)이라 부른다. 가전기기의 중요 소음 발생원이 유체소음, 전자기소음, 기계적소음, 연소소음등 소음원의 종류에 따라 저소음기술을 해석하는데 상당한 차이가 있다. 따라서 사용조건별 설정기준을 정하고 설정기준에 따른 현상소음 lavel보다 약 10dBA보다 낮은 소음 목표치로 설계되어야 한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.2
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• pp.139-146
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• 2021

In hybrid rocket combustion, the oxidizer swirl injection is frequently used to stabilize the combustion as the rotational velocity component affects the boundary layer flow. However, as the swirl strength increases, a problem arises where the combustion performance changes too much. Thus, this study attempts to control the low frequency instability while minimizing the change in combustion performance by adapting attenuated swirl injection with fuel insert used in reference [7]. To this end, a series of experimental tests were performed by varying swirl intensity and the location of the fuel insert. In the tests, the occurrence of combustion instability and combustion performance were closely monitored. The results confirmed that combustion instability was successfully suppressed at the condition of the swirl angle 6 degree and the location of fuel insert 310 mm. And, the changes in combustion pressure, O/F ratio, and fuel regression rate were found as minimal compared to the baseline case. Also the results reconfirmed that the formation of positive coupling between two high frequency oscillations in 500 Hz band, combustion pressure(p') and heat release oscillation(q'), is the necessary and sufficient condition of the occurrence of low frequency instability.

• Journal of Energy Engineering
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• v.20 no.2
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• pp.163-169
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• 2011

This research is to decide the possibility of using RM50(reformulated methanol fuel) without any modification of engine by the method of numerical analysis. Comparing the heat release rate, the difference among each fuel was decreased according to the increase of the engine speed, and the maximum heat release rate was higher in the order of RM50 and gasoline fuel. Also, this order corresponds to the order of burning speed. RM50 had the higher turbulent burning speed, and the curve of turbulent intensity was showed similar tendency to the curve of turbulent burning speed. RM50 had relatively high burning speed, short quenching length, high temperature in cylinder, so that it might increase NO emission, but owing to chemical reaction dynamics, it was decreased NO emission. Therefore, in order to predict the possibility of using RM50, it is needed to consider not only the temperature in cylinder by low heating value, but also combustion characteristics including burning speed.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.46 no.12
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• pp.1021-1027
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• 2018

Experimental studies have been conducted to verify that the positive coupling between pressure oscillation (p') and combustion oscillation (q') of high frequency range is a prerequisite for the initiation of low frequency instability in hybrid rocket combustion. The post-chamber length and combustion equivalence ratio were selected as critical parameters to control the phase difference between p' and q', and p' amplitude in relation to the suppression of LFI. In the results, even if the post-chamber length increases, the phase difference between p' and q' maintains below pi/2, which is a necessary condition for the LFI development, but the amplification of RI (Rayleigh index) was substantially decreased leading to a stable combustion. In addition, results confirmed that combustion stability is achieved by changing the momentary equivalence ratio and/or by suppressing the positive coupling status of p' and q'. Thus, the periodic amplification of RI was identified as the middle path of the mechanism of occurrence of LFI.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.9 no.2
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• pp.221-228
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• 1997

A strong combustion-driven sound from a surface burner made of a perforated metal fiber plate for premixed gas was investigated to clarify the physical mechanism of its generation. A simple model was developed for the acoustic power generation in terms of the heat transfer response function and the acoustic impedance of the burner. The acoustic impedance of the perforated metal fiber placed on the open exit was measured and the heat release response of the burner to the oscillating flow associated with the acoustic disturbance was expressed in terms of a response function. It was found that the power is generated by the heat release in response to the downstream particle velocity, in contrast to the upstream velocity in the case of the Rijke oscillation driven by a heater placed in the lower half of a columm with upstream flow. The measured frequencies of the oscillation were in agreement with the estimated resonance frequencies and their excitation was varied with the combustion conditions. For the same fuel rate, the excited frequency increases with the air ratio if it is low but decreases with the ratio if not so low. Such frequency characteristics were explained by assuming a heat release response function with a time constant and it was shown that the excited frequency decreases as the time constant increases.

• Journal of the Korean Society of Combustion
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• v.3 no.1
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• pp.59-69
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• 1998

The results of study on the active control of naturally occurring combustion oscillations with a single dominant frequency in an atmospheric dump combustor are presented. Control was achieved by an oscillatory infection of secondary fuel at the dump plane. A high speed solenoid valve with a maximum frequency of 250Hz was used as the actuator and a sound level meter, located at the combustor exit, measured the pressure fluctuations which served as the feedback signal for the control loop. Instability characteristics were mapped over a range of mean mixing section velocities from 6.7 m/s-9.3 m/s and with three mixing conditions. Different fuel/air mixing conditions were investigated by introducing varying percentages of primary fuel at two locations, one at the entrance to the mixing section and one 6 mixing tube diameters upstream of the dump plane. Control studies were conducted at a mean velocity of 9.3 m/s, with an air temperature of $415^{\circ}C$, and from flame blowout to the stoichiometric condition.