• Title/Summary/Keyword: Pressure Propagation

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Development and Application of an Explosion Modeling Technique Using PFC (PFC3D에서의 폭원모델링 기법의 개발 및 적용)

  • Choi Byung-Hee;Yang Hyung-Sik;Ryu Chang-Ha
    • Explosives and Blasting
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    • v.22 no.4
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    • pp.7-15
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    • 2004
  • An explosion modeling technique was developed by using the spherical discrete element code, PFC3D, which can be used to model the dynamic stress wave propagation phenomenon. The modeling technique is simply based on an idea that the explosion pressure should be applied to a PFC3D particle assembly not in the form of an external force (body force), but in the form of a contact force (surface force). According to this concept, the explosion pressure is applied to the wall particles by the scheme of radius expansion/contraction of inner-hole particles. The output wall force is compared to the input hole pressure in every time step, and a correction routine is activated to control the radius multiplier of the inner-hole particles. A comparative blast simulation far a cement mortar block of $80\times90\times80mm$ was conducted by using the conventional explosion modeling method and the new one. The results of the simulation are presented in a qualitative fashion.

Observation of Discharge Mode Transient from Townsend to Glow at Breakdown of Helium Atmospheric Pressure Dielectric Barrier Discharge (헬륨 대기압 유전체 격벽 방전기의 타운젠트-글로우 방전 모드 전이 연구)

  • Bae, Byeongjun;Kim, Nam-Kyun;Yoon, Sung-Young;Shin, Jun-Seop;Kim, Gon-Ho
    • Journal of the Semiconductor & Display Technology
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    • v.15 no.2
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    • pp.26-31
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    • 2016
  • The Townsend to glow discharge mode transition was investigated in the dielectric barrier discharge (DBD) helium plasma source which was powered by 20 kHz / $4.5 kV_{rms}$ high voltage at atmospheric pressure. The spatial profile of the electric field strength at each modes was measured by using the intensity ratio method of two helium emission lines (667.8 nm ($3^1D{\rightarrow}2^1P$) and 728.1 nm ($3^1S{\rightarrow}2^1P$)) and the Stark effect. ICCD images were analyzed with consideration for the electric field property. The Townsend discharge (TD) mode at the initial stage of breakdown has the light emission region located in the vicinity of the anode. The electric field of the light emitting region is close to the applied field in the system. Immediately, the light emitting region moves to the cathode and the discharge transits to the glow discharge (GD) mode. This mode transition can be understood with the ionization wave propagation. The electric field of the emitting region of GD near cathode is higher than that of TD near anode because of the cathode fall formation. This observation may apply to designing a DBD process system and to analysis of the process treatment results.

Effect of Airborne Noise from Ship Machinery on Underwater Noise (선박의 장비 공기소음이 수중소음에 미치는 영향)

  • Kim, Hyun-Sil;Kim, Jae-Seung;Kim, Bong-Ki;Kim, Sang-Ryul;Lee, Seong-Hyun
    • Journal of the Society of Naval Architects of Korea
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    • v.48 no.6
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    • pp.569-574
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    • 2011
  • In research vessels or naval ships, airborne noise from machineries such as diesel engine is the major source of underwater noise at low speed. In this paper, effect of engine noise on underwater noise is studied by considering two paths; sound radiation from hull plate and direct airborne noise transmission through hull plate. SEA (Statistical energy analysis) is used to predict hull plate vibration induced by engine noise, where SEA model consists of only two subsystems; engine room air space and hull plate. The pressure level in water is calculated from sound radiation by plate. Engine noise transmission through hull plate is obtained by assuming plane wave propagation in air-limp plate-water system. Two effects are combined and compared to the measurement, where speaker is used as a source in engine room and sound pressure levels in engine room and water are measured. The hydrophone is located 1 m away from the hull plate. It is found below 1000 Hz, prediction overestimates underwater sound pressure level by 5 to 12 dB.

Ignition Characteristics of Combustion Chamber with $LO_X$ Lead Cyclogram for Liquid Rocket Engine (액체로켓엔진 연소기 산화제 선공급 Cyclogram에 의한 점화특성)

  • Han, Yeoung-Min;Kim, Jong-Gyu;Lee, Kwang-Jin;Lim, Byoung-Jik;Ahn, Kyu-Bok;Kim, Mun-Ki;Seo, Seong-Hhyeon;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.137-142
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    • 2008
  • Ignition characteristics of combustion chamber with LOx lead cyclogram for liquid rocket engine were described. The combustion chamber has chamber pressure of 60 bar, propellant mass flow rate of 89 kg/s, and nozzle expansion of 12. Cold flow test to determine the filling time of propellant for cyclogram with LOx lead supply, ignition test to check the ability to ignite starting fuel from the ignitor, low pressure combustion test to check the propagation of flame into main fuel-oxidizer mixture from starting fuel and the main combustion stage, and design point combustion test to check the combustion performance were performed. Ignition and combustion tests with LOx lead supply were successfully performed and the stable cyclogram of start sequence for combustion chamber was developed.

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Solar Radiation Pressure Model Comparison for GPS Satellites (GPS 궤도의 태양풍 모델 비교)

  • Yu, Seon-Gyeong;Kim, Gang-Ho;Kee, Chang-don;Heo, Mun-Beom
    • Journal of Advanced Navigation Technology
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    • v.22 no.6
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    • pp.585-590
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    • 2018
  • GPS satellite orbits could be estimated precisely using GPS dynamics as well as GPS observations. Most of the perturbations are available to be generated using satellite position, velocity, well known model equations and coefficients. However, who wants to calculate solar radiation pressure (SRP) should choose a SRP model and estimate the coefficients of a SRP model. The accuracy of SRP model depends on the model characteristics. Therefore this paper has estimated coefficients of SRP models using CODE precise orbit product and compared the accuracy of orbit propagator depending on SRP model. The results show that the extended CODE orbit model (ECOM) and the reduced ECOM achieved cm level fitting orbit for the CODE 1-day orbit. Also orbit propagation model without SRP model consideration could get tens of meter orbits compared to CODE orbits.

Study of the Compressive Behavior of Polypropylene-low Glass Fiber Compound and Thermoplastic Olefin under High Strain Rate (고 변형률 속도에서 폴리프로필렌 및 열가소성 올레핀 소재의 압축 거동에 대한 연구)

  • Lee, Se-Min;Kim, Dug-Joong;Han, In-Soo;Kim, Hak-Sung
    • Composites Research
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    • v.35 no.1
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    • pp.38-41
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    • 2022
  • In this study, the strain rate dependent tensile and compressive properties of PP-LGF and TPO was investigated under the high strain rate by using the Split Hopkinson Pressure Bar (SHPB). The SHPB is the most widely used apparatus to characterize dynamic mechanical behavior of materials at high strain rates between 100 s-1 and 10,000 s-1. The SHPB test is based on the wave propagation theory which was developed to give the stress, strain and strain rate in the specimen using the strains measured in the incident and transmission bars. In addition, to verify the strain data obtained from SHPB, the specimen was photographed with a high-speed camera and compared with the strain data obtained through the Digital Image Correlation (DIC).

Evaluation of Internal Blast Overpressures in Test Rooms of Elcetric Vehicles Battery with Pressure Relief Vents (압력배출구를 설치한 전동화 차량 배터리 시험실의 내부 폭압 평가)

  • Pang, Seungki;Shin, Jinwon;Jeong, Hyunjin
    • Journal of the Korean Society for Geothermal and Hydrothermal Energy
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    • v.18 no.3
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    • pp.7-18
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    • 2022
  • Secondary batteries used in electric vehicles have a potential risk of ignition and explosion. Various safety measures are being taken to prevent these risks. A numerical study was performed using a computational fluid dynamics code on the cases where pressure relief vents that can reduce the blast overpressures of batteries were installed in the through-compression test room, short-circuit drop test room, combustion test room, and immersion test room in facilities rleated to battery used in electric vehicles. This study was conducted using the weight of TNT equivalent to the energy release from the battery, where the the thermal runaway energy was set to 324,000 kJ for the capacity of the lithium-ion battery was 90 kWh and the state of charge (SOC) of the battery of 100%. The explosion energy of TNT (△HTNT) generally has a range of 4,437 to 4,765 kJ/kg, and a value of 4,500 kJ/kg was thus used in this study. The dimensionless explosion efficiency coefficient was defined as 15% assuming the most unfavorable condition, and the TNT equivalent mass was calculated to be 11 kg. The internal explosion generated in a test room shows the very complex propagation behavior of blast waves. The shock wave generated after the explosion creates reflected shock waves on all inner surfaces. If the internally reflected shock waves are not effectively released to the outside, the overpressures inside are increased or maintained due to the continuous reflection and superposition from the inside for a long time. Blast simulations for internal explosion targeting four test rooms with pressure relief vents installed were herein conducted. It was found that that the maximum blast overpressure of 34.69 bar occurred on the rear wall of the immersion test room, and the smallest blast overpressure was calculated to be 3.58 bar on the side wall of the short-circuit drop test room.

Effect of ZnO Nanoparticle Presence on SCC Mitigation in Alloy 600 in a Simulated Pressurized Water Reactors Environment

  • Sung-Min Kim;Woon Young Lee;Sekown Oh;Sang-Yul Lee
    • Journal of the Korean institute of surface engineering
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    • v.56 no.6
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    • pp.401-411
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    • 2023
  • This study investigates the synthesis, characterization, and application of zinc oxide (ZnO) nanoparticles for corrosion resistance and stress corrosion cracking (SCC) mitigation in high-temperature and high-pressure environments. The ZnO nanoparticles are synthesized using plasma discharge in water, resulting in rod-shaped particles with a hexagonal crystal structure. The ZnO nanoparticles are applied to Alloy 600 tubes in simulated nuclear power plant atmospheres to evaluate their effectiveness. X-ray diffraction and X-ray photoelectron spectroscopy analysis reveals the formation of thermodynamically stable ZnCr2O4and ZnFe2O4 spinel phases with a depth of approximately 35 nm on the surface after 240 hours of treatment. Stress corrosion cracking (SCC) mitigation experiments reveal that ZnO treatment enhances thermal and mechanical stability. The ZnO-treated specimens exhibit increased maximum temperature tolerance up to 310 ℃ and higher-pressure resistance up to 60 bar compared to non-treated ZnO samples. Measurements of crack length indicate reduced crack propagation in ZnO-treated specimens. The formation of thermodynamically stable Zn spinel structures on the surface of Alloy 600 and the subsequent improvements in surface properties contribute to the enhanced durability and performance of the material in challenging high-temperature and high-pressure environments. These findings have significant implications for the development of corrosion-resistant materials and the mitigation of stress corrosion cracking in various industries.

The Properties of Microwave Propagation in Discharging Plasma (방전에 의한 프라즈마에서의 마이크로파 전파특성)

  • Yang, In-Eung;No, Bang-Hyeon;Kim, Bong-Yeol
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.5 no.3
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    • pp.31-39
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    • 1968
  • In this paper microwave power propagated through the cold plasma was analyzed and measured with respect to the external magenetic flux density. The d. c discharge plasma was in the rectangular waveguide in which two electrode was inserted, and also the glass diseharge tube inserted in the ractangular wavegside. The direction of microwave pro-pagation, the axis of the discharge tube and external magnetic flux were perpendicular to each other. It showed that the attenuation and absorption of micro wave power propagated in the plasma was increased as the magnetic flux density, the discharge current and the pressure of the gas were increased.

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Experimental Study on the Flow Characteristics in a Low Speed Research Compressor (연구용 저속 축류압축기의 내부 유동 특성에 관한 실험적 연구)

  • Park, Tae-Choon;Han, Jung-Youp;Kang, Shin-Hyoung
    • The KSFM Journal of Fluid Machinery
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    • v.11 no.6
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    • pp.54-63
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    • 2008
  • A study on the flow characteristics in a 4-stage axial compressor and the behavior of rotating stall was experimentally performed at the third-stage rotor and stator rows in order to investigate its performance and instability of the compression system. The pressure losses generated due to the leakage flow at a tip clearance and a shroud seal clearance and the wake flow near the trailing edge of a blade were taken into consideration to estimate the causes of performance drop of the low speed research compressor(LSRC) in Seoul national university. In addition, the measurement of rotating stall was conducted with hot-wire probes and the existence and propagation of stall cell could be confirmed through fast Fourier transform and cross-correlation analysis.