• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.45-52
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• 2008

In order to investigate the initiation and propagation processes of a spherical detonation wave induced by direct initiation, numerical simulations were carried out using two-dimensional compressible Euler equations with an axisymmetric assumption and a one-step reaction model based on Arrhenius kinetics with various levels of ignition energy. By varying the amount of ignition energy, three typical initiation behaviors, which were subcritical, supercritical and critical regimes, were observed. Then, the ignition energy of more than $137.5{\times}10^6$ in non-dimensional value was required for initiating a spherical detonation wave, and the minimum ignition energy(i.e., critical energy) was less than that of the one-dimensional simulation reported by a previous numerical work. When the ignition energy was less than the critical energy, the blast wave generated from an ignition source continued to attenuate due to the separation of the blast wave and a reaction front. Therefore, detonation was not initiated in the subcrtical regime. When the ignition energy was more than the minimum initiation energy, the blast wave developed into a multiheaded detonation wave propagating spherically at CJ velocity, and then a cellular pattern radiated regularly out from the ignition center in the supercritical regime. The influence on ignition energy was observed in the cell width near the ignition center, but the cell width on the fully developed detonation remained constant during the expanding of detonation wave due to the consecutive formation of new triple points, regardless of ignition energy. When the ignition energy was equal to the critical energy, the decoupling of the blast wave and a reaction front appeared, as occurred in the subcrtical regime. After that, the detonation bubble induced by the local explosion behind the blast wave expanded and developed into the multiheaded detonation wave in the critical regime. Although few triple points were observed in the vicinity of the ignition core, the regularly located cellular pattern was generated after the onset of the multiheaded detonation. Then, the average cell width on the fully developed detonation was almost to that in the supercritical regime. These numerical results qualitatively agreed with previous experimental works regarding the initiation and propagation processes.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2005년도 제25회 추계학술대회논문집
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• pp.136-140
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• 2005

일차원 ZND 데토네이션 구조 해석 모델의 연장선상에서 경사 충격파와 경사 데토네이션 파에 대하여 Rankine-Hugoniot 관계식과 반응속도를 연계한 이차원 경사 데토네이션 파의 구조해석 모델을 제시하였다. 이에 기반을 두어 삼중점, 횡단 충격파 및 셀 구조를 포함하는 경사 데토네이션 파의 비정상 상세 구조를 조사하기 위한 이차원 유체역학 해석을 수행하였다. 전산 유체 해석 결과는 경사 데토네이션 파의 상세구조에 대한 깊이 있는 이해를 제공하며, 해석 모델은 경사 데토네이션 파를 연소 메커니즘으로 이용하는 극초음속 추진기관의 통합 설계도구로 이용될 수 있을 것이다.

• 오토저널
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• 제7권1호
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• pp.48-54
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• 1985

One of the most probable reason of the apex seal damage in IR-2500 industrial Wankel (rotary) engine was believed to be the engine detonation. Both analytical and experimental studies were made with a view th find out engine detonation pressure. The stagnation detonation pressure $p_{03}$' was estimated based on the data from IR-2500 engine detonation tests, such as engine firing pressure, state of fresh charge at BDC and polytropic compression exponent. The estimated stagnation detonation pressure for the natural gas fueled IR-2500 engine was in excess of 3,700 psia. With natural gas liquid added to the natural gas the octane value of the fuel was lowered, thus, making the engine more prone to detonate. The estimated detonation pressure for the case with the mixed fuel was about 3,400 psia which was sufficiently high to break the apex seal. The subsequent engine lab tests performed on two identical engines with sole difference in the apex seal thickness between the two engines proved that the engine knock, in fact, was the villain of the apex seal failure.ilure.

• 한국터널지하공간학회 논문집
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• 제10권2호
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• pp.185-191
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• 2008

본 연구에서는 정밀한 초시설정이 가능한 전자뇌관을 이용하여 터널에서의 다단 시차 분할발파(OBM)를 실시하며 대형 대단면 지하 공간 창출 요구에 발맞추어 기존뇌관(비전기뇌관)과의 비교를 통해 진동 소음 저감효과와 시공성, 효율성을 비교 검토하자 하였다. 본 연구를 통해 전자뇌관 적용 시 진동 소음 제어 및 비산거리, 여굴량, 파쇄입도가 비전기뇌관가 비교하여 양호한 결과를 나타냄을 확인할 수 있었다.

• 한국화재소방학회논문지
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• 제22권3호
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• pp.228-233
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• 2008

폭굉한계는 가연성물질의 화재 및 폭발 위험성을 결정하기 위해 사용되는 중요한 연소 특성치 가운데 하나이다. 본 연구에서는 가연성혼합물의 구성하는 각 순수성분의 연소열과 기상 조성을 이용하여 폭발한계를 예측하였다. 제시된 방법론에 의한 계산값은 적은 오차범위에서 문헌값과 일치하였다. 따라서 본 연구에서 제시한 방법론이 다른 가연성물질의 폭굉한계 예측에 폭넓게 적용되기를 기대한다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2006년도 제32회 KOSCO SYMPOSIUM 논문집
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• pp.205-212
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• 2006

Three-dimensional numerical study was carried out for the investigation of the detonation wave structures propagating in tubes. Fluid dynamics equations and conservation equation of reaction progress variable were analyzed by a MUSCL-type TVD scheme and four stage Runge-Kutta time integration. Chemical reaction was modeled by using a simplified one-step irreversible kinetics model. The variable gas properties between unburned and burned states were considered by using variable specific heat ratio formulation. The unsteady computational results in three-dimension show the detailed mechanisms of rectangular and diagonal mode of detonation wave instabilities resulting same cell length but different cell width in smoked-foil record. The results for the small reaction constant shows the spinning mode of three-dimensional detonation wave dynamics, which was rarely observed in the previous numerical simulation of the detonation waves.

• International Journal of Aeronautical and Space Sciences
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• 제16권4호
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• pp.548-559
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• 2015

We performed a numerical simulation based on the two-dimensional (2-D) unsteady Euler's equation with a single-step Arrhenius reaction model in order to investigate the detonation wave front propagation of an Argon (Ar) diluted oxy-hydrogen mixture ($2H_2+O_2+12Ar$). This simulation operates in the detonation frame of reference. We examine the effect of grid size and the performance impact of integrated quantities such as mass flow. For a given set of baseline conditions, the minimal and maximum grid resolutions required to simulate the respective detonation waves and the detonation cell structures are determined. Tertiary shock wave behavior for various grids and pre-exponential factors are analyzed. We found that particle fluctuation can be weakened by controlling the mass flow going through the oblique shock waves.

• 한국안전학회지
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• 제11권4호
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• pp.64-71
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• 1996

Detonation phenomena of $C_2H_2$were invesgated using the various shock tube. To study the detonation characteristics according to the composition of $C_2H_2-0_2$$_2$ and $C_2H_2$-air mixtures, the composition were varied from 5 to 90% and 5 to 50% of acetylene each other. A spiral ring was installed in the shock tube to study the effect of obstacles in DDT phenomena. Detonation velocities were measured using the photodiode, and the DDT phenomena was visualized using the high speed schlieren photograph. From the experimental result, it was found that the detonation velocity was most high near the 1. 8times the stoichiometric ratio of acetylene. And from the visualization of DDT phenomena, it was found that the detonation wave was strengthened throuth the pile up of small compression wave of burned gas. And the obstacles in shock tube accelerate the detonation reaction by turblent effect of flammable gas mixture.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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• pp.275-278
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• 2012

We investigate the interaction between the propagation of detonation and inserted gaps in the high explosive. The Eulerian-based multi-material simulation code validated through comparison with experimental results was used. A series of gap materials is used to understand the detonation propagation characteristic in the presence of multiple gaps.

• 한국추진공학회지
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• 제12권3호
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• pp.68-75
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• 2008

이전에 개발된 병렬 해석 코드를 이용하여 원형 관내에서의 삼차원 데토네이션 파 전파 특성을 관찰 하였다. 일련의 해석을 통하여 직경이 일정한 원형 관에서 반응 속도 상수 값 k에 의존하는 데토네이션 셀 생성 메커니즘을 알 수 있었다. 삼차원 유동에 대한 비정상 유동의 해석 결과는 two-, three-, four-cell 구조의 메커니즘을 잘 보여주었으며, 반응속도 상수 k가 증가함에 따라 생성되는 셀 수가 증가하고 셀의 폭과 길이는 감소하였다. 모든 다중-셀 모드에서 데토네이션 파의 구조와 그을음막 기록은 횡단파의 움직임에 의하여 만들어지며, 데토네이션 파면은 주기적으로 일정한 다각형 및 풍차 형상을 가지게 된다.