• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.358-363
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• 2008

The spray cross-section characteristics of two-phase spray that using external-mixing nozzle injected into a subsonic cross flow were experimentally studied with various ALR ratio that is $0{\sim}59.4%$. Suction type wind tunnel was used and experiments were conducted to ambient environment. Several plain orifice nozzles with L/d of 30 and orifice diameter of 0.5 mm and orifice length 1.5 mm were tested. Free stream velocity profiles at the injection location were measured using hot wire. Spray images were captured to study collision point and column trajectory. Phase Doppler particle analyzer(PDPA) was utilized to quantitatively measuring droplet SMD, volume flux. Measuring probe of PDPA positions was moved 3-way transverse machine. SMD distributions were layered structure and peaked at the top of the spray plume and low value at bottom of the spray. Volume flux of spray was distributed to the two side region and volume flux quantity decreased when ALR ratio increased. It was found that the perpendicularly injected two-phase spray jet of external mixing into a cross flow showing that mistlike spray moved away from the test section bottom region.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 제33회 추계학술대회논문집
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• pp.399-402
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• 2009

로켓엔진 연소기의 음향 불안정 억제를 위해 헬름홀츠 공명기의 음향학적 최적 설계 설계조건을 실험적, 해석적으로 연구하였다. 표준 음향시험 절차에 따라 음향파관에 공명기를 장착하여 음향파응답 신호를 측정하였다. 측정된 신호를 토대로, 흡음계수를 계산하였고, 이로부터 공명기의 음향감쇠 성능을 파악하였다. 헬름홀츠 공명기를 스프링-댐퍼 시스템으로 상사하여, 음향학적 감쇠성능을 이해하였다. 헬름홀츠 공명기의 설계변수로 목의 길이와 공동의 크기 등을 선택하였다. 공동의 크기가 커질수록 흡음성능이 증가하였고, 목 길이가 길어질수록 흡음성능이 감소하였다.

• 대한기계학회논문집B
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• 제20권3호
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• pp.1005-1014
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• 1996

An experimental investigation has been carried out to examine the influence of injector design variables and operating conditions on the resultant drop size for triplet impinging streams injectors. The variables studied in this investigation are pressure drop, impinging angle, orifice length to diameter ratio, and impinging point distance. Droplet-size data are obtained using water as the propellant simulant by Malvern Particle Analyzer System. Drop size decreases with increasing impinging angle and pressure drop while other injector parameters remain constant at the same point. But it is found that there is no noticeable droplet-size change which results from change in orifice length to diameter ratio or impinging point distance within the investigated range.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년도 제31회 추계학술대회논문집
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• pp.82-85
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• 2008

액체로켓엔진에서 고주파 연소불안정의 제어를 위해 연소 안정화 장치인 음향공을 적용하여, 제한된 공간에서 유동장의 특성과 설계인자에 따른 감쇠효과를 연구하였다. 연소 불안정을 모사하기 위하여 제한된 공간에 압력 진동 장치를 이용하여 공진을 발생시켜, 음향공의 장착에 따른 감쇠 효과를 측정하였다. 유동장의 특성중 하나인 유속을 변화시키기 위하여 유량을 변화시켰으며, 설계인자로는 음향공 오리피스의 직경과 길이를 변화시켜 연구를 수행하였다. 유동장 하에서의 음향공 장착에 따른 감쇠효과를 확인 하였으며, 오리피스 길이와 직경이 작을 경우 유속 증가에 따라서 음향공의 튜닝이 오른쪽(고주파수)으로 이동하는 현상을 확인하였다.

• Journal of Korean Neurosurgical Society
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• 제58권6호
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• pp.499-503
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• 2015

Objective : The transradial catheterization (TRC) is becoming widespread, primarily for neurointerventions. Therefore, the evaluation of radial artery puncture in clinical practice and a better understanding of the anatomy are important to improve the safety of neuroendovascular surgery. Methods : Ten formalin-fixed adult Korean cadavers were dissected to expose radial artery (RA), brachial artery (BrA) and subclvian artery (ScA), bilaterally. Vessel lengths and diameters were meaured using a caliper and distance between the specific point of vessels and the anatomical landmarks including the radial styloid process, the medial epicondyle of the humerus, the sternoclavicular joint, and the vertebral artery orifice were also measured. Results : The average length between the radial (RAPS) and the BrA puncture sites (BrAPS) and between the vertebral artery orifice (VAO) and the BrA bifurcation (BrAB) did not differ between sides (p>0.05). The average length between the radial styloid process (RSP) and the RAPS was $13.41{\pm}2.19mm$, and the RSP was $26.85{\pm}2.47mm$ from the median nerve (MN). The mean length between the medial epicondyle (ME) and the BrAPS as $44.23{\pm}5.47mm$, whereas the distance between the ME and the MN was $42.23{\pm}4.77mm$. The average VAO-ScA angle was $70.94{\pm}6.12^{\circ}$, and the length between the ScA junction (SCJ) and the VAO was $60.30{\pm}8.48mm$. Conclusion : This study provides basic anatomical information about the radial artery and the brachial route and can help improving new techniques, selection of size and shape of catheters for TRC. This can help neurointerventionists who adopt a transradial neuroendovascular approach and offers comprehensive and safe care to their patients.

• 설비공학논문집
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• 제7권3호
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• pp.501-511
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• 1995

A numerical model for predicting the performance of gas distrubutor type double inlet pulse tube refrigerators has been developed. The model was based on adiabatic analysis and the losses of heat exchangers and regenerator were considered. Thermodynamic behavior of working fluid within a double inlet pulse tube refrigerator was investigated and the effects of design parameters, such as valve and orifice openings, cold heat exchanger temperature, frequency and pulse tube length, on the cooling capacity and COP were shown.

• 설비공학논문집
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• 제25권7호
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• pp.377-385
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• 2013

In this study, the performance of an impeller according to blade length and pitch angle was studied experimentally by building a variable pitch impeller while changing blade length to review the effect of blade length and pitch angle on a fan's performance. The pitch angle was changed in six steps from $20^{\circ}{\sim}45^{\circ}$ at intervals of $5^{\circ}$ while the blade lengths were changed to 90 mm, 100 mm, 110 mm and 120 mm with an identical airfoil shape while carrying out the experiment. The results are summarized as follows : The air flow per static pressure of axial fans increased linearly with increase of pitch angle, but the high static pressure showed a decrease at a pitch angle of $35^{\circ}$. The shaft power increased proportionally to the pitch angle at all blade lengths; the larger the pitch angle, the larger the measured increase of shaft power. This is because the drag at the fan's front increases with the pitch angle. In the axial fans considered in this research, the flow and incre.

• Anatomy and Cell Biology
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• 제56권1호
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• pp.61-68
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• 2023

Anatomical knowledge of the occipital condyle (OC) and its relationships to surrounding structures is important for avoiding injury during craniovertebral junction (CVJ) surgeries. This study was conducted to evaluate the morphology and morphometry of OC and its relationship to foramen magnum, jugular foramen (JF), and hypoglossal canal (HC). Morphometric parameters including length, width, height, and distances from the OC to surrounding structures were measured. The oval-like condyle was the most common OC shape, representing for 33.0% of all samples. The mean length, width and height of OC were 21.3±2.4, 10.5±1.4, and 7.4±1.1 mm, respectively. Moreover, OC was classified into three types based on its length. The most common OC length in both sexes was moderate length or type II (62.5%). The mean distance between anterior tips and posterior tips of OC to basion, and opisthion were 11.5±1.4, 39.1±3.3, 25.2±2.2, and 27.4±2.7 mm, respectively. The location of intracranial orifice of HC was commonly found related to middle 1/3 of OC in 45.0%. JF was related to the anterior 2/3 of OC in 81.0%, the anterior 1/3 of OC in 12.5%, and the entire OC length in 6.5%. These morphological analysis and morphometric data should be taken into consideration before performing surgical operation to avoid CVJ instability and neurovascular structure injury.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2009년도 춘계학술대회 논문집
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• pp.253-256
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• 2009

350Kw급 이하의 초소형 터보제트엔진에서 연료 미립화 특성을 만족하는 분사시스템을 개발하는 것은 매우 어려운 일이다. 그러나 회전 연료 분사시스템은 복잡한 고압연료펌프 시스템 없이도 엔진축의 원심력만을 이용함으로써 좋은 미립화를 할 수 있다. 이러한 이유로, 직경 40 mm의 매우 작은 회전식 연료 인젝터를 제작하였으며, 여러 가지 크기의 분사 오리피스에 대한 실험을 수행하였다. PDPA 측정 시스템을 사용하여 입자의 크기와 속도, 분무분포를 측정하였다. 실험 결과, 분사 오리피스로부터 분출된 단일 액주의 길이는 회전속도에 의해 제어되며, SMD는 회전수가 증가함에 따라 감소하고, 오리피스의 직경과 오리피스 내부에 생성되는 액막두께에 큰 영향을 받는다.

• 한국가스학회지
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• 제13권5호
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• pp.7-14
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• 2009

본 연구는 석탄화력발전소 노의 연소효율 향상을 위하여 미분탄 수송배관의 공기-입자 유동장의 압력손실 특성을 분석하여 미분탄 수송장치 내에 설치되어 유량을 제어하는 오리피스의 설계에 적용하고자 하는 것이다. 통상의 미분탄 수송배관장치는 관의 형태에 따라 직선관, 곡선관 및 엘보우로 구성된다. 본 연구에서는 공기유동과 입자운동의 상호작용 해석을 통하여 직선관과 곡선관을 갖는 미분탄 수송배관장치 내의 압력손실을 분석하였다. 총 압력손실은 공기-미분탄 입자의 마찰 손실 증가와 배관의 길이, 곡선관 각도의 증가에 따라 증가하는 것으로 확인되었다. 연구결과로 압력손실과 유량제어를 위한 최적화된 오리피스 설계 프로그램이 개발되었으며 그 계산 결과를 기존의 실험결과와 비교, 분석하였다.