• 한국추진공학회지
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• 제17권2호
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• pp.9-15
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• 2013

Shchelkin 나선으로 알려진 나선형 난류고리가 아세틸렌-산소 혼합기의 데토네이션파의 성능에 미치는 영향을 실험적으로 연구하였다. 고속응답 압력 트랜스듀서로 측정된 압력 피크의 시간차를 이용하여 데토네이션파 속도를 산출하였다. 또한 추력대를 이용해 데토네이션파의 강도를 측정하여 나선형 난류고리가 연소성능에 미치는 영향을 분석하였다. CFD를 이용하여 간접적으로 유량을 산출하고, 최대 충진률을 위한 최소 충진시간을 도출하였다. 아세틸렌-산소 추진제의 당량비 2.4에서 최대속도 및 압력을 나타냈으며, CEA로 계산된 C-J 속도와 유사한 값을 보였다. 짧은 연소기와 짧은 나선형 난류고리를 사용하는 경우에 최대의 데토네이션파 속도를 나타냈지만, 반대로 난류고리를 사용하지 않은 긴 연소기에서 최대 추력성능을 보였다.

• 한국연소학회:학술대회논문집
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• 한국연소학회 2012년도 제45회 KOSCO SYMPOSIUM 초록집
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• pp.97-99
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• 2012

A pressure-based BOIK model considering Shock to Detonation Transition(SDT) and damage due to external fragment or bullet stimuli impact on energetic materials and analytical approach for determination of free parameters are proposed. The rate of product mass fraction(${\lambda}$) consists of ignition term that represents the initiation due to shock compression and growth term that describes propagation of detonation wave and strain term representing the morphological deformation induced by external impact.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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• pp.314-318
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• 2006

연소파를 이용한 로켓 점화장치 등에의 응용으로 관내에서 전파되는 데토네이션에 대한 관심이 증대되고 있으나 그 특성에 관하여 알려진 바는 많지 않다. 본 실험적 연구에서는 프로판-산소 혼합기로 채워진 직경 5mm, 길이 30m의 투명한 관을 이용하여 데토네이션 파의 진행을 고속촬영을 통하여 가시화하였다. 평균 속도를 측정한 결과, 압력이 감소함에 따라 정상적인 Chapman-Jouguet(CJ) 모드에서 약 $0.5V_{CJ}$에 이르는 저속 모드로 평균 속도가 감소하는 천이 영역이 존재한다. 관 길이 전체에 걸쳐 데토네이션 전파의 동적 특성을 관찰한 결과, 천이 영역에서는 데토네이션이 매우 불안정하여 주기적이거나 간헐적인 속도의 출렁임이 발생한다.

• 한국안전학회지
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• 제6권2호
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• pp.31-36
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• 1991

Quenching effects of acetylene and hydrogen into oxygen detonation by using detonation arrester ［DA］are studied in this paper. The experiments were carried out in cylinderical shock tube. 5m long, 30mm dia., with stolchlometric ratio ［SR］of each gas and 10-l20$\mu$ Cell Size of brass and Stainless Steel of DAs were installed in it To clarify arresting ability correlation with initial pressure, Pi, critical thickness, Tct, and shapes of supporting panel of DA are also investigated It is found that ­detonation velocities has most dependency on Pi, it shows notable changes around 0.5kgf/$\textrm{cm}^2$ for hydrogen, 0.15kgf/$\textrm{cm}^2$ for acetylen respectively, ­DA can be safety device able to arrest shock wave of detonation, ­over Tct flame transmission might be only the factor has to be considered, ­acetylene seems to be much more stronger detonation characteristics than hydrogen because of reaction heat.

• Journal of Mechanical Science and Technology
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• 제15권12호
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• pp.1822-1828
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• 2001

The experiment for the sympathetic detonation (Sudo et al., 1951) (Fukuyama et al., 1958) in water was conducted. Composition B (RDX: 64%, TNT: 36%, Detonation velocity: 7900m/s) was used for both donor (the thickness was 50mm, and the diameter was 31mm) and receptor charges. The distance between the donor and the receptor, and the thickness (5, 7.5, 10mm) of the receptor were varied in the experiments. In order to investigate the basic characteristics of the underwater sympathetic detonation of high explosive, the sympathetic detonation phenomena were visualized by a high-speed camera (HADLAND PHOTONICS, IMACON790) in forms of streak and framing photographs. The 200ns/mm streak velocity was 2㎲. Manganin gauges (KYOWA Electronic INSTRUMENTS CO. SKF-21725) were used for the pressure measurements. The gauges were set under the receptor. The pressures during the complete and incomplete explosions were measured.

• 한국연소학회:학술대회논문집
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• 대한연소학회 2003년도 제27회 KOSCO SYMPOSIUM 논문집
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• pp.153-157
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• 2003

Supersonic and hypersonic aircrafts must pass wide range of speed to reach high speed region. But for existing engines the most efficient operating speed ranges are decided according to their flying speed, so an engine which mixes several engines like TRJ (Turbo Ramjet) and ARJ (Air Turbo Ramjet) has been planed. This mixed type engine has inefficiency that more than two engines must be installed simultaneously, but the pulse detonation engine (PDE) that uses detonation wave has a strong point that it can operate in all speed range with single engine. This paper deals with the simulation of the pulse detonation engine which uses hydrogen peroxide $(H_2O_2)$ mono propellant. Hydrogen peroxide is low-cost propellant, and it is reacted without oxidizer. Comparison between $H_2-O_2$ mixture with $H_2O_2$ mono propellant about thrust, pressure, temperature and velocity shows that $H_2O_2$ is a very useful propellant.

• 한국항공우주학회지
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• 제42권10호
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• pp.858-869
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• 2014

대부분의 항공우주 추진은 정압 Brayton 사이클에 기초하고 있으나 성능 향상을 위한 압력비 증가는 기계적 한계에 직면하고 있다. 지난 십여 년간 고속 추진에 적합한 연소방식으로 기대 받은 데토네이션 추진이, 최근에는 추진기관과 동력 장치의 열효율을 획기적으로 증대시켜 줄 수 있는 "game-changer"로 연구되고 있다. 즉, 데토네이션 파에 수반하는 강한 충격파의 압축 효과는 기존의 압축 방식에서 얻기 힘든 열효율을 증가시키는 것으로 여겨진다. 본 논문에서는 펄스데토네이션엔진의 최신 기술 동향과 더불어 정적연소에 기초한 압력증가연소 체계의 연구 동향에 대하여 소개할 것이다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 1998년도 춘계 학술대회논문집
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• pp.1-14
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• 1998

Underwater explosion properties for TNT, an ideal explosive, and DXD-04, a nonideal explosive, were numerically modeled with a one-dimensional Lagrangian hydrodynamic code. The equation of state parameters for detonation products for TNT and DXD-04 were obtained from the BKW code, assuming complete reaction. Burn of TNT was modeled by using the Chapman-Jouguet(CJ) volume burn technique, a programmed-burn technique, assuming instantaneous detonation reaction. Burn of DXD-04 was modeled by using the same technique and by using the reaction rate calibrated from two-dimensional steady-state detonation experiments. The calculations for TNT reproduced the experimental peak pressure of the shock wave propagating through water with an error of $3.0\%$ and the experimental oscillation period of the bubble formed of detonation products with an error of $2.3\%$. For DXD-04, the CJ volume burn technique could not reproduce the experimental observations. When the reaction rate calibrated from two-dimensional steady-state detonation experimental data, the calculated peak pressure was slightly higher by $7.3\%$ than the experimental data, but the calculated shock profile was in good agreement. The bubble period was reproduced with an error of $1.8\%$. These results demonstrated that underwater explosion properties for an ideal explosive can be predicted by using a programmed burn technique, and that, however, those for a nonideal explosive can be predicted only when a well-calibrated reaction rate is used.

• 한국터널지하공간학회 논문집
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• 제5권4호
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• pp.337-348
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• 2003

밀장전한 암반 발파공에서 화약 폭발시 발생하는 고압의 폭굉압력 전파메카니즘을 충격파 이론을 적용하여 규명하고 전달된 발파압력 산정식을 유도하였다. 유도된 발파압력 산정식은 폭굉파속도, 단열지수, 화약밀도, Hugoniot 상수, 암반밀도의 함수였다. 에멀젼 화약과 서울 화강암의 특성시험을 시행하여 각 특성치의 확률분포를 정의하고 발파압력 산정식에 적용하여 발파압력의 확률분포를 산출하였다. 화약 특성치와 암반 특성치의 확률분포는 정규분포를 나타냈으며 따라서 발파압력의 확률분포도 정규분포로 추정되었다. 발파압력에 대한 매개변수분석을 시행한 결과 폭굉파속도가 발파압력에 가장 크게 영향을 미쳤다. 또한 이런 특성치의 불확실성이 발파압력의 불확실성에 미치는 영향을 분석하였다. 분석결과 암반특성치의 불확실성이 화약특성치보다 더 크게 영향을 미쳤다. 비록 매개변수분석에서 폭굉파속도가 발파압력에 가장 크게 영향을 미치는 요소이지만 암반특성치의 불확실성이 폭굉파속도의 불확실성보다 더 크기 때문에 발파압력은 후자보다 전자에 의해서 더 크게 영향을 받는다.

• Geomechanics and Engineering
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• 제14권6호
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• pp.545-552
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• 2018

Blast-induced ground vibrations by a significant amount of explosives may cause many problems for mining slope stability. Geological discontinuities have a significant influence on the transmission of dynamic pressure of detonation and according to their position relative to the slope face may have damaging or useful impacts on the slope stability. In this study, the effect of geological discontinuities was investigated by modelling a slope with geological discontinuities through applying the dynamic pressure in three-dimensional discrete element code (3DEC). The geological discontinuities in four states that generally apperceived in mine slopes are considered. Given the advantages of the pressure decay function defined by some researcher, this type of function was used to develop the pressure-time profile. The peak particle velocities (PPV) values were monitored along an axis by utilization of Fish programming language and the results were used as an indicator to measure the effects. As shown in the discontinuity-free model, PPV empirical models are reliable in rocks lacking discontinuities or tightly jointed rock masses. According to the other results, the empirical models cannot be used for the case where the rock mass contains discontinuities with any direction or dip. With regard to PPVs, when the direction of discontinuities is opposite to that of the slope face, the dynamic pressure of detonation is significantly damped toward the slope direction at the surface of discontinuities. On the other hand, when the discontinuities are horizontal, the dynamic pressure of detonation affects the rock mass to a large distance.