• 항공우주기술
• /
• 제12권1호
• /
• pp.163-172
• /
• 2013

본 논문에서는 전산유동해석 기법을 활용하여 액체 로켓 연소 후류에 냉각수가 분사됨에 따라 발생하는 냉각 효과를 냉각수 분사량, 분사 위치, 분사 방식의 변화에 따른 영향을 고찰하였다. 연소 후류의 모사를 위해서는 동결 유동해석 기법에 기반한 단일화학종 비반응 해석 모델을 이용하였고, 연소 후류에 분사된 냉각수의 모사를 위해서는 Euler-Lagrangian 해석법에 따르는 이산 상 모델(Discrete Particle Model)을 사용하였다. 해석 결과 연소 후류의 약 2배 정도 냉각수가 투입되었을 때 연소 후류 중심부에서는 연소 후류의 온도가 상대적으로 감소하는 것을 확인할 수 있었다.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
• /
• pp.179-182
• /
• 2007

현재 예비설계가 진행 중인 새로운 다목적실용위성은 자세 및 궤도조정을 위해 4.45 N의 단일추진제 추력기를 장착할 예정이다. 본 논문에서는 추력기 작동시 분출되는 플룸이 위성에 미치는 영향을 살펴보기 위해 직접모사법(Direct Simulation Monte-Carlo Method)을 이용해 3차원 위성체 기저부 형상에 대해 수치해석을 수행하였고, 이를 통해 플룸의 온도 및 밀도 분포와 태양 전지판으로의 복사열전달 양을 예측하였다.

• 한국안전학회지
• /
• 제37권6호
• /
• pp.166-173
• /
• 2022

A variety of input parameters are taken into consideration while performing a Level 3 PSA. Some parameters related to plume segments, spatial grids, and particle size distribution have flexible input formats. Fine modeling performed by splitting a number of segments or grids may enhance the accuracy of analysis but is time-consuming. Analysis speed is highly important because a considerably large number of calculations is required to handle Level 2 PSA scenarios for a single-unit or multi-unit Level 3 PSA. This study developed a sensitivity analysis supporting interface called MACCSsense to compare the results of the trials of plume segmentation with the results of the base case to determine its impact (in terms of time and accuracy) and to support the development of a modeling approach, which saves calculation time and improves accuracy. MACCSense is an automation tool that uses a large amount of plume segmentation analysis results obtained from MUST Converter and Mr. Manager developed by KAERI to generate a sensitivity report that includes impact (time and accuracy) by comparing them with the base-case result. In this study, various plume segmentation approaches were investigated, and both the accuracy and speed of offsite consequence analysis were evaluated using MACCS as a consequence analysis tool. A simultaneous evaluation revealed that execution time can be reduced using multi-threading. In addition, this study can serve as a framework for the development of a modeling strategy for plume segmentation in order to perform accurate and fast offsite consequence analyses.

• 설비공학논문집
• /
• 제15권12호
• /
• pp.1018-1027
• /
• 2003

This study treats the analysis of the performance and the design of plume abatement wet/dry cooling tower with dry type heat exchanger using a numerical method. A two-dimensional analysis is performed using the finite volume method for mechanical draft counterflow and crossflow tower. For a coupling problem between water and air system, a turbulent two phase flow is considered. Effectiveness-NTU method is used for modeling of the dry type heat exchanger. The parameter change simulations of the outer wall shape, the relative flowrate of air, and attachment of an air mixer are performed to examine the effect on plume abatement. It is found that if the relative air flowrate ratio and the adequate air mixer type are chosen well in addition to the ratio of water to air flowrate, the loss of the cooling capacity and the additional cost are reduced and the plume is abated.

• International Journal of Air-Conditioning and Refrigeration
• /
• 제13권2호
• /
• pp.61-70
• /
• 2005

This study treats the numerical analysis of performance and design for plume abatement wet/dry cooling tower with a dry type heat exchanger. A two-dimensional analysis is performed using the finite volume method for mechanical draft counterflow and crossflow tower. For a coupling problem between water and air system, a turbulent two phase flow is considered. The Effectiveness-NTU method is used for modeling of the dry type heat exchanger. The parametric simulations such as the relative flowrate of air and attachment length of an air mixer are performed to examine the effect on plume abatement. It is found that if the relative air flowrate ratio and the adequate air mixer type are chosen well in addition to the ratio of water to air flowrate, the loss of cooling capacity and the additional cost are reduced and the plume is abated.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 1999년도 추계 학술대회논문집
• /
• pp.65-70
• /
• 1999

Radiative heating of a liquid rocket base plane due to plume emission is numerically investigated. Calculation of flow and temperature fields around rocket nozzle precedes and thereby realistic plume shape and temperature distribution inside the plume are obtained. Based on the calculated temperature field, radiative transfer equation is solved by discrete ordinate method. The averaged radiative heat flux reaching the base plane is about $5kW/m^2$ at the flight altitude of 10.9km. This value is small compared with radiative heat flux caused by constant-temperature (1500K) plume emission, but it is not negligibly small. At higher altitude (29.8km), view factor between the babe plane and the exhaust plume is increased due to the increased expansion angle of the plume. Nevertheless, the radiative heating disappears since the base plane is heated to high temperature (above 1000K) due to convective heat transfer.

• 한국항공우주학회지
• /
• 제32권8호
• /
• pp.118-128
• /
• 2004

화염에 의한 종방향 공력 특성의 변화를 해석하기 위하여 고형 화염 모형을 이용한 풍동 시험과 고형 화염 모형과 제트 화염 모델을 이용한 난류 유동 수치 해석을 실시하였다. 화염 경계면 근사 가법을 이용하여 산출한 형상을 본떠 화염 모형을 제작하였으며 제트 화염 모델링 기법을 이용하여 공기와 실제 화염의 열역학적 차이로 인한 오차를 보정한 공기 제트 화염을 생생하였다. 화염과 외부 공기의 간섭에 대해 난류 모델간의 비교를 통하여 정확도와 격자 의존성 등에서 Spalart-Allmaras 모델이 좋은 결과를 주었다. 수치 해석을 통하여 고형 화염 모형과 제트 화염의 차이를 분석하였으며, 실제 비행 시험에 대한 화염 영향을 분석하기 위하여 연소실과 대기 압력 비와 레이놀즈수에 따른 변화를 해석하였다.

• 대한원격탐사학회:학술대회논문집
• /
• 대한원격탐사학회 2006년도 Proceedings of ISRS 2006 PORSEC Volume I
• /
• pp.118-121
• /
• 2006

Variations in the extent and dispersal of river plume are important in the study of coastal environment. The objectives of this study are to examine relationship between satellite detected plume area and river discharge and to clarify the temporal and spatial dynamic of plume from Tokachi River, Hokaido, Japan. We used 1.1 km spatial resolution of SeaWiFS normalized water-leaving radiance (nLw) images from 1998 to 2002. Supervised maximum likelihood classification was implemented to define classes of surface water optical properties. Satellite observed plume area was correlated to the amount of river discharge from April to October. First mode (44% of variance) of EOF analysis shows the turbid plume distribution resulting from re-suspension by strong wind mixing along the coast during winter. This mode also shows plume distribution along-shelf direction in spring and late summer. Second mode (17% of variance) shows spring pattern across-shelf direction due to strong discharge of snow melting water.

• 한국항공우주학회지
• /
• 제40권8호
• /
• pp.688-694
• /
• 2012

본 연구에서는 엔진 노즐 형상이 엔진 Plume의 적외선 신호 특성에 미치는 영향에 대해서 연구하였다. 이를 위해 적외선 신호 감소 효과를 가지는 큰 세장비의 엔진 노즐과 적외선 감소가 요구되지 않는 항공기에 적용되는 일반적인 원통형 형상의 노즐에 대한 형상설계를 수행하였다. 그리고 두 노즐에 대한 열유동해석을 수행하고 두 노즐의 유동장 특성을 비교하였다. 이후 열유동해석 결과를 이용하여 두 노즐에 대한 적외선 신호 해석을 수행하고 그 결과를 분석하였다.

• Journal of Advanced Marine Engineering and Technology
• /
• 제20권5호
• /
• pp.93-102
• /
• 1996

Laser-induced plume and laser-target interaction during pulsed laser deposition are demonstrated for a lead zirconate titanate (PZT). A KrF excimer laser (wavelength 248nm) was used and the laser was pulsed at 20Hz, with nominal pulse width of 20ns. The laser fluence was~$16J/cm^2,$ with 100mJ per pulse. The laser-induced plasma plume for nanosecond laser irradiation on PZT target has been investigated by optical emission spectra using an optical multichannel analyzer(OMA) and by direct observation of the plume using an ICCD high speed photography. OMA analysis showed two distinct ionic species with different expansion velocities of fast or slow according to their ionization states. The ion velocity of the front surface of the developing plume was about $10^7$cm/sec and corresponding kinetic energy was about 100eV. ICCD photograph showed another kind of even slower moving particles ejected from the target. These particles considered expelled molten parts of the target. SEM morphologies of the laser irradiated targets showed drastic melting and material removal by the laser pulse, and also showed the evidence of the molten particle ejection. The physics of the plasma(plume) formation and particle ejection has been discussed.