• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2008년 추계학술대회논문집
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• pp.367-373
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• 2008

Spinning detonations propagating in a circular tube were numerically investigated with a one-step irreversible reaction model governed by Arrhenius kinetics. Activation energy is used as parameter as 10, 20, 27 and 35, and the specific heat ratio and the heat release are fixed as 1.2 and 50. The time evolution of the simulation results was utilized to reveal the propagation mechanism of single-headed spinning detonation. The track angle of soot record on the tube wall was numerically reproduced with various levels of activation energy, and the simulated unique angle was the same as that of the previous reports. The maximum pressure histories of the shock front on the tube wall showed stable pitch at Ea=10, periodical unstable pitch at Ea=20 and 27 and unstable pitch consisting of stable, periodical unstable and weak modes at Ea=35, respectively. In the weak mode, there is no Mach leg on the shock front, where the pressure level is much lower than the other modes. The shock front shapes and the pressure profiles on the tube wall clarified the mechanisms of these stable and unstable modes. In the stable pitch at Ea=10, the maximum pressure history on the tube wall remained nearly constant, and the steady single Mach leg on the shock front rotated at a constant speed. The high and low frequency pressure oscillations appeared in the periodical unstable pitch at Ea=20 and 27 of the maximum pressure history. The high frequency was one cycle of a self-induced oscillation by generation and decay in complex Mach interaction due to the variation in intensity of the transverse wave behind the shock front. Eventually, sequential high frequency oscillations formed the low frequency behavior because the frequency behavior was not always the same for each cycle. In unstable pitch at Ea=35, there are stable, periodical unstable and weak modes in one cycle of the low frequency oscillation in the maximum pressure history, and the pressure amplitude of low frequency was much larger than the others. The pressure peak appeared after weak mode, and the stable, periodical unstable and weak modes were sequentially observed with pressure decay. A series of simulations of spinning detonations clarified that the unsteady mechanism behind the shock front depending on the activation energy.

• 한국추진공학회지
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• 제12권2호
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• pp.66-73
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• 2008

본 논문에서는 환형 관에서의 데토네이션 파의 전파 특성을 살펴보았다. 이전의 연구에 이용된 수치 기법과 이동 계산 창 기법을 본 연구에 이용하였으며, 관 폭의 값으로 무차원화 된 곡률 반경을 유일한 기하학적 변수로 고려하여 일련의 해석을 수행하였다. 곡률 반경이 작은 환형 관에서 데토네이션 파는 불안정하여 정규적인 데토네이션 셀 구조가 나타나지 않으며 셀 구조가 유지될 수 있는 임계 곡률 반경이 존재함을 알 수 있었다. 곡률의 효과로 관의 내벽 및 외벽은 압력 차가 발생하며, 외벽 쪽에 서는 overdriven 데토네이션의 경향을 가진다. 예상할 수 있는 바와 같이 곡률 반경이 커지면서 직선관의 결과에 수렴한다.

• 한국추진공학회지
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• 제22권3호
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• pp.81-89
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• 2018

본 연구에서는 소형 추력기 및 점화기로 활용 가능한 소형 PDE의 작동특성을 실험적으로 알아보았다. 4.22 mm의 내경을 갖는 상용 가스 튜브를 이용하여 소형 PDE를 구성하였으며, 당량비 및 작동 주파수 변화에 따른 PDE의 작동 및 데토네이션 전파 특성을 알아보았다. 측정된 데토네이션 속도는 1 Hz와 5 Hz 작동 조건에서는 희박 영역을 제외한 당량비 조건에 이론값과 10%이내의 오차를 가지는 비교적 정확한 값을 보였다. 그러나 20 Hz 조건의 희박 영역에서는 불안정한 전파 특성을 보였으며, 20~62%의 큰 속도 결손이 발생하였다.

• Journal of applied mathematics & informatics
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• 제6권2호
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• pp.631-638
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• 1999

Sensitive testing has been widely employed for many years in connection with the development and evaluation explosives detonation devices and propellants. Perhaps its earliest and possibly most important implementation was in biological studies of dosage mortality and response to drugs. Recently sensitivity experiments has been employed in the evaluation of new materials subject to stress in various environments and in delineanation of unstable combustion regions in chemical propulsion systems. This paper discussed a sta-tistical development of sensitivity testing.

• 한국연소학회지
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• 제7권1호
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• pp.23-30
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• 2002

Instability of oblique detonation waves (ODW) at off-attaching condition was investigated through a series of numerical simulations. Two-dimensional wedge of finite length was considered in $H_2/O_2/N_2$ mixtures at superdetonative condition. Numerical simulation was carried out with a compressible fluid dynamics code and a detailed hydrogen-oxygen combustion mechanism. Present result reveals that there is a chemical kinetic limit of the ODW detachment, in addition to the theoretical limit predicted by Rankine-Hugoniot theory with equilibrium chemistry. Result also presents that ODW still attaches at a wedge as an oblique shock-induced flame showing periodically unstable motion, if the Rankine-Hugoniot limit of detachment is satisfied but the chemical kinetic limit is not. Mechanism of the periodic instability is considered as interactions of shock and reaction waves coupled with chemical kinetic effects. From the investigation of characteristic chemical time, condition of the periodic instability is identified as follows; at the detaching condition of the Rankine-Hugoniot theory, (1) flow residence time is smaller than the chemical characteristic time, behind the detached shock wave with heat addition, (2) flow residence time should be greater than the chemical characteristic time, behind an oblique shock wave without heat addition.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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• pp.32-33
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• 2003

Mechanism of a periodic oscillation of shock-induced combustion over a two- dimensional wedges and axi-symmetric cones were investigated through a series of numerical simulations at off-attaching condition of oblique detonation waves(ODW). A same computational domain over 40 degree half-angle was considered for two-dimensional and axi-symmetric shock-induced combustion phenomena. For two-dimensional shock-induced combustion, a 2H2+02+17N2 mixture was considered at Mach number was 5.85with initial temperature 292 K and initial pressureof 12 KPa. The Rankine-Hugoniot relation has solution of attached waves at this condition. For axi-symmetric shock-induced combustion, a H2+2O2+2Ar mixture was considered at Mach number was 5.0 with initial temperature 288 K and initial pressure of 200 mmHg. The flow conditions were based on the conditions of similar experiments and numerical studies.[1, 3]Numerical simulation was carried out with a compressible fluid dynamics code with a detailed hydrogen-oxygen combustion mechanism.[4, 5] A series of calculations were carried out by changing the fluid dynamic time scale. The length wedge is varied as a simplest way of changing the fluid dynamic time scale. Result reveals that there is a chemical kinetic limit of the detached overdriven detonation wave, in addition to the theoretical limit predicted by Rankine-Hugoniot theory with equilibrium chemistry. At the off-attaching condition of ODW the shock and reaction waves still attach at a wedge as a periodically oscillating oblique shock-induced combustion, if the Rankine-Hugoniot limit of detachment isbut the chemical kinetic limit is not.Mechanism of the periodic oscillation is considered as interactions between shock and reaction waves coupled with chemical kinetic effects. There were various regimes of the periodicmotion depending on the fluid dynamic time scales. The difference between the two-dimensional and axi-symmetric simulations were distinct because the flow path is parallel and uniform behind the oblique shock waves, but is not behind the conical shock waves. The shock-induced combustion behind the conical shockwaves showed much more violent and irregular characteristics.From the investigation of characteristic chemical time, condition of the periodic instability is identified as follows; at the detaching condition of Rankine-Hugoniot theory, (1) flow residence time is smaller than the chemical characteristic time, behind the detached shock wave with heat addition, (2) flow residence time should be greater than the chemical characteristic time, behind an oblique shock wave without heat addition.

• 화약ㆍ발파
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• 제40권3호
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• pp.19-32
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• 2022

수소는 다른 연료에 비해 에너지효율이 높고 유해물질이 배출되지 않아 미래의 청정에너지원으로 인식되고 있다. 그러나 수소는 밀도가 낮아 운반 및 저장시에 부피가 커서 압축하거나 특별한 운반체를 사용해야 하며, 공기중에 노출 시 화재나 폭발의 위험성이 있다. 수소-공기 혼합물의 폭발에 관한 실험이나 수치해석적 연구가 진행되어 오고 실물 수소 충전소를 대상으로 한 폭발 시뮬레이션에 관한 연구사례는 극히 드물다. 본 연구에서는 실제 수소 충전소를 대상으로 Lidar 스캐닝을 수행하여 point cloud 데이터를 획득하고 수소 충전소 3 차원 구조 모델을 작성한다. 3 차원 구조모델은 Ansys 사 AUTODYN 에 적용되어 수소 충전소의 수소폭발을 가정한 TNT 등가량의 폭발 시뮬레이션을 실시하고 주변에 전파하는 폭발압력을 계산하여, 수소 충전소 폭발에의한 주변 보안 건물의 안전거리에 관한 정보를 제공한다.