• Title/Summary/Keyword: deflector

Search Result 123, Processing Time 0.021 seconds

A Computational Study on Cooling Analysis of the Flame Deflector for the 75 tonf Class Propulsion Test Facility (75톤급 추진기관 시험설비 화염유도로 냉각해석에 관한 수치적 연구)

  • Moon, Seong-Mok;Cho, Nam-Kyung;Kim, Seong-Lyong;Jun, Sung-Bok;Lee, Kyoung-Hoon;Kim, Dong-Hwan
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.19 no.2
    • /
    • pp.55-64
    • /
    • 2015
  • In this study, a 3-D flame cooling analysis is conducted to examine thermal safety for the flame deflector of the 75 tonf class propulsion test facility, and the safe discharge of the exhaust gas is assessed by using numerical results. The Mixture multiphase model is adopted for the simulation of heat transfer and phase exchange process between flame and cooling water, and the computational study using the single species unreacted model for the exhaust plume is carried out for the flame cooling. Numerical analysis predicts maximum temperature on the flame deflector wall for different water flow rates, and evaluates the safe minimum flow rate of water corresponding to the fire-resistant temperature for concrete.

Analysis of Primary Breakup Characteristics Depending on the Boss and Deflector Dimension of Fire Sprinkler Head using LES-VoF (LES-VoF를 이용한 소방용 스프링클러 헤드의 보스 및 디플렉터 치수에 따른 1차 분열 특성 분석)

  • Kim, Taehoon
    • Journal of ILASS-Korea
    • /
    • v.26 no.3
    • /
    • pp.127-134
    • /
    • 2021
  • Fire sprinkler initial spray was analyzed by Large eddy simulation (LES) and Volume of Fluid (VoF) integrated method. The IsoAdvector geometric VoF was used to identify the liquid-gas interface clearly even with the large Courant-Friedrichs-Lewy number. To reduce the computational costs, sector meshes and Adaptive Mesh Refinement up to level 3 were used. Base mesh size was 1 mm, which is roughly equivalent to the initial sprinkler droplet. Top surface radius of boss and deflector size were modified to investigate the effects of sprinkler head design on primary breakup process. When top surface radius of boss was increased, vertical liquid sheet was formed. This phenomenon reduced the sheet breakup radius, sheet thickness and velocity. Due to reduced liquid sheet thickness, a large amount of ligaments was created from the liquid sheet. As a result, there was a dramatic decrease in volume per surface area, indicating an increase in breakup process. Spray pattern viewed in radial direction also changed when top surface radius of boss increased. When top surface radius of boss was increased, a T-shaped pattern was observed while a V-shaped pattern was observed in all other cases. When the deflector size increases, the spray pattern remains V-shaped, even if the top surface radius of boss increased. Further studies on promoting atomization of the water supplied to the lower part of the sprinkler head in the T-shape pattern should be conducted.

A Study on Determination for Location of Localizer Antenna under Area Restrictive Conditions at Domestic P-Airport (국내 P공항의 부지 제한조건을 고려한 로컬라이저의 최적위치 선정에 관한 연구)

  • Cho, Hwan-Kee;Kim, Jong-Bum;Song, Byung-Heum
    • Journal of the Korean Society for Aviation and Aeronautics
    • /
    • v.23 no.2
    • /
    • pp.7-14
    • /
    • 2015
  • This paper deals with an optimal determination process for the built-in location of localizer under restrictive siting area conditions of a domestic P-airport. Aerodynamic forces and moments acting on the localizer structure can be used a reference to find the safe distance from jet blast and the position at which the reasonable structural loading is applied. Wind tunnel experiment is conducted to measure aerodynamic loadings. The finite element analysis for structural deformation is employed to get the information of structural failure. A new localizer's position is determined by considering aerodynamic loading, structural strength and thermal loading due to jet blast. Deflector effect was also investigated in this study. In conclusion, the location of localizer can be placed at shorter than the current position and greatly decreased if the deflector is applied at the front of localizer.

CFD Investigation of Rocket Nozzle Plume for Flame Deflector Preliminary Analysis (화염유도로 예비 해석을 위한 로켓노즐 플룸의 CFD 해석 검증)

  • Jun, Doo-Sung;Kim, Jae-Woo;Kim, Jong-Rok;Kim, Woo-Kyeom;Kim, Seung-Cheol;Moon, Hee-Jang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2011.11a
    • /
    • pp.313-316
    • /
    • 2011
  • This paper investigates CFD investigation on single phase supersonic nozzle flow and 2-phase subson ic flow prior to rocket nozzle supersonic 2-phase flow with water injection within the flame deflector. Numerical results of supersonic nozzle single phase flow showed no notable unrealistic behavior as it captures the usual shock cell structures. Three-dimensional 2-phase flow analysis has also been performed to verify whether the approach can grab the droplet behavior during cooling by water injection. It is expected these basic studies will enhance the cooling problem analysis of supersonic 2-phase rocket plume in the future.

  • PDF

Evaluation of Hydraulic Characteristics Influenced by Different Deflector Baffles in the Sedimentation Basin with Inclined Plate Settler (경사판 침전지에서 저류벽의 설치위치에 따른 수리학적 특성의 평가)

  • Yu, Myong-Jin;Kim, Hyun-Chul;Ryu, Seong-Ho
    • Journal of Korean Society on Water Environment
    • /
    • v.21 no.1
    • /
    • pp.40-45
    • /
    • 2005
  • Sedimentation is one of the most common and important units in conventional water treatment plant. Structure such as various baffle walls and inclined plate settler may be obstacles to the horizontal flow when it is poorly designed. Therefore, the effects of these structures on characteristics of hydraulic flow must be evaluated to improve the settling efficiency of the floc. The hydraulic characteristic of the two sedimentations at Y water treatment plant (YWTP), which have different deflector baffles inside the settling basin, were investigated by tracer (fluoride) test. The inclined plate settler installed inside settling basin caused an undesirable impact on horizontal flow and produced dead zone. Solid baffle wall under the plate settler could help to minimize the formation of density currents and flow short circuiting. NaF used as a tracer was recovered more than 90% at investigated all basins. Morill index ($t_{90}/t_{10}$), Modal index ($t_p/T-HRT$) and short-circuiting index ($[M-HRT-t_p]/M-HRT$) were determined from tracer test results performed at YWTP. Those indices ranged 2.95~3.02, 0.40~0.53 and 0.32~0.46, respectively.

Temperature and Pressure Measurement on the Flame Deflector during KSLV-I Flight Tests (나로호 비행시험을 통한 화염유도로의 온도 및 압력 측정)

  • Jung, Il-Hyung;Moon, Kyung-Rok;Kang, Sun-Il;An, Jae-Chel;Ra, Seung-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.39 no.4
    • /
    • pp.378-384
    • /
    • 2011
  • During the flight test of KSLV-I, various sensors are installed in the launch pad and the flame deflector to measure the flame characteristics and their influences on the launch complex when a launch vehicle lifts off. Parameter Measurement System is responsible for acquiring the above flight test data. The measurement methodology such as the configuration of measurement system, sensor locations and data acquisition procedures are presented. And this paper compares and explains the characteristics of data sets measured during two flight tests.

Improvement of Maldistributed Air Velocity in the Vane Wheel of a Bowl Type Pulverizer (바울형 미분기 베인휠에서의 유속 불균일 개선에 관한 연구)

  • Park, Deok-Bae;Hur, Jin-Huek;Moon, Seung-Jae
    • Plant Journal
    • /
    • v.6 no.2
    • /
    • pp.62-69
    • /
    • 2010
  • The stability of coal pulverizer in the 800 MW coal-fired plants is vital to maintain their performance. Thus, this study analyzed the uneven abrasion of the deflector and coal spillage due to the air velocity maldistribution in the vane wheel of a bowl-type pulverizer as it is a possible cause for problems of facility using pulverized coal. In addition, air flow in the underbowl of a bowl-type pulverizer was studied to check air velocity maldistribution in the vane wheel using numerical method. In an attempt to correct the maldistribution of air velocity, air flow of the modified duct vane was studied as enlarging the length of the duct vanes installed at the air inlet duct of the pulverizer and increasing the angle of inclination. It was found that modified duct vane make the velocity distribution at the vane wheel uniform. formed by the duct vanes installed at the air inlet duct of the pulverizer and swirling flow is the major factor in making the velocity distribution of vane wheel exit uniform. This can prevent the uneven abrasion of the deflector, which is one of the components inside the pulverizer and coal spillage.

  • PDF

Design Study for Pulsed Proton Beam Generation

  • Kim, Han-Sung;Kwon, Hyeok-Jung;Seol, Kyung-Tae;Cho, Yong-Sub
    • Nuclear Engineering and Technology
    • /
    • v.48 no.1
    • /
    • pp.189-199
    • /
    • 2016
  • Fast neutrons with a broad energy spectrum, with which it is possible to evaluate nuclear data for various research fields such as medical applications and the development of fusion reactors, can be generated by irradiating proton beams on target materials such as beryllium. To generate short-pulse proton beam, we adopted a deflector and slit system. In a simple deflector with slit system, most of the proton beam is blocked by the slit, especially when the beam pulse width is short. Therefore, the available beam current is very low, which results in low neutron flux. In this study, we proposed beam modulation using a buncher cavity to increase the available beam current. The ideal field pattern for the buncher cavity is sawtooth. To make the field pattern similar to a sawtooth waveform, a multiharmonic buncher was adopted. The design process for the multiharmonic buncher includes a beam dynamics calculation and three-dimensional electromagnetic simulation. In addition to the system design for pulsed proton generation, a test bench with a microwave ion source is under preparation to test the performance of the system. The design study results concerning the pulsed proton beam generation and the test bench preparation with some preliminary test results are presented in this paper.

Investigation of Exhaust Facility of Liquid Rocket Propulsion System (액체로켓 추진기관의 후류처리장치 고찰)

  • Cho, Nam-Kyung;Lee, Kwang-Jin;Han, Young-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2012.05a
    • /
    • pp.133-138
    • /
    • 2012
  • Exhaust facility has basically the role of flame deflector, and considering additional functions, it can be classified by noise/emission suppressor and altitude simulation facility. In this paper, principles of flame deflector, jet pump, emission suppression are presented for exhaust treatment facility. Principles of noise suppression caused by Mach wave mitigation, jet energy mitigation by water evaporation and condensation are shown. In addition, a concept of vertical exhaust treatment facility is presented applying basic principles aforementioned.

  • PDF

A Convergent Investigation on the Air flow in Driving According to a Cargo Container and the Wind Deflector (트럭 화물칸 및 윈드 디플렉터에 따른 운행중 공기흐름에 대한 융합 연구)

  • Choi, Kye-Kwang;Cho, Jae-Ung
    • Journal of the Korea Convergence Society
    • /
    • v.11 no.9
    • /
    • pp.175-180
    • /
    • 2020
  • In this study, the freight vehicles were modelled and the flow analysis on the existence or non-existence of a cargo container and the wind deflector were carried out. Based on the driving speed of 100 km/hr, at all models A, B and C, the highest flow rate was shown between 58 m/s and 59 m/s at the top of the model shape. All models A, B and C showed the highest pressure of air resistance between 652Pa and 671Pa at the front of the model geometry. The maximum pressure of model A is considered to be the smallest, with the least flow resistance to speed compared to models B and C. Therefore, it can be seen that model A has an advantageous condition for air resistance in terms of fuel costs. Unlike model B which causes the rapid flow resistance at the cargo compartment, model C can be found to flow a little more smoothly on the streamlined wind deflector. So, the flow air at a streamlined shape is considered to be more advantageous in terms of air resistance than at angular shape. By applying the research analysis result on the air flow in driving according to a cargo container and the wind deflector, it is seen that this study is adequate at the practical efficient design and aesthetic convergence.