• Title/Summary/Keyword: Envelope Condition

Search Result 104, Processing Time 0.022 seconds

Design of Vessel Assembly for Fuel Irradiation Test in Reactor (원자로 내 핵연료조사시험용 압력용기조립체 설계)

  • Park, Kook-Nam;Lee, Jong-Min;Chi, Dae-Young;Park, Su-Ki;Lee, Chung-Young;Kim, Young-Jin
    • Proceedings of the KSME Conference
    • /
    • 2004.11a
    • /
    • pp.383-387
    • /
    • 2004
  • The Fuel Test Loop (FTL) consists of In-Pile Test Section (IPS) and Out-of-Pile System (OPS). The test condition in IPS such as pressure, temperature and quality of the main cooling water, can be controlled by the OPS. The FTL has been developed to be able to irradiate three pins to the core irradiation hole (IR1 hole) by considering for its utility and user's irradiation requirement. The IPS vessel assembly (IVA) consists of IPS head, outer pressure vessel, inner pressure vessel, inner assembly and test fuel carrier. The IVA is approximately 5.6 m long and fits within a 74 mm in diameter envelope over the full height of the chimney. Above the top of the chimney, the head of the IPS is enlarged to allow the closure flanges and pipe work connections. IVA was designed to test the CANDU and PWR nuclear fuel pin together. Specially, wished to minimize interference by nuclear fuel change in design and synthesize these items and shape design for IVA.

  • PDF

Design and Manufacture of Storage Air Heater (축열식 가열기의 설계 및 제작)

  • Lee, Yang-Ji;Kang, Sang-Hun;Park, Poo-Min;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2006.11a
    • /
    • pp.43-46
    • /
    • 2006
  • Storage air heater(SAH) is a general purpose facility that is used to simulate the high altitude condition of supersonic ground test facility, thurst compensation test of rocket engine nozzle and gas turbine engine combustor test. SAH in KARI is built to simulate the total temperature of the supersonic ground test facility which has a wide flight envelope from altitude 0km, Mach 2 to altitude 25km, Mach 5 and operates up to 1300K, 3.5MPa. In this paper, we introduces the SAH in JAXA which is model of SAH in KARI and summarizes the design process and manufacture of ours.

  • PDF

Preliminary Design of Movable Ramjet Intake (가변 초음속 흡입구 기본설계)

  • Lee, Kyung-Jae;Kang, Sang-Hun;Lee, Yang-Ji;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2008.05a
    • /
    • pp.207-210
    • /
    • 2008
  • In this study, one type of ramjet intake were designed for the flight condition of Mach number 4 and numerical analysis was performed. In order to widen the flight envelope range (Mach number $2{\sim}6$), movable intake concept was applied. The central body was designed so that the capture area ratio which is one of most important factors of ramjet intake design could be adjusted. And various types of cowl and movable insert part of shell were designed in order to control throat area which could increase total pressure recovery. The numerical results showed that the designed ramjet intake could be applied in various flights Mach number.

  • PDF

Full Rig Test and High Altitude Ignition Test of Micro Turbojet Engine Combustor (초소형 터보제트엔진 연소기의 리그시험 및 고고도 점화시험)

  • Lee, Dong-Hun;Kim, Hyung-Mo;Park, Poo-Min;You, Gyung-Won;Paeng, Ki-Suk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2009.05a
    • /
    • pp.373-376
    • /
    • 2009
  • A full rig combustor test and altitude ignition test were carried out for radial-annular combustor of micro turbojet engine. 11.2% total pressure loss and 99.85% of combustion efficiency were measured at design point of engine under sea level standard condition and $2{\sim}6$ of air excess ratio for ignition envelope was achieved on engine starting regime. Finally, A 30,000 ft high altitude ignition test was also performed and finally we found out that the developed radial-annular combustor is appropriate to micro turbojet engine.

  • PDF

A Study on the Simulation of Natural Ventilation Effect for Single-sided Casement Window as Opening Types (케이스먼트 창호 개폐방식에 따른 자연환기 효과에 관한 시뮬레이션 연구)

  • Choi, Taehwoan;Kim, Taeyeon;Leigh, Seung-Bok
    • KIEAE Journal
    • /
    • v.7 no.4
    • /
    • pp.57-62
    • /
    • 2007
  • At the moment, the reduction of building energy consumption is a unavoidable task of mankind for conserving global environment. Decreasing overall U-value of building envelope and air infiltration, especially in Korean climate condition with clear four seasons, are the obvious solutions for the objective. Thus low glazing ratio with small window openings are required for heating and cooling load reduction in buildings. Using larger window openings could provide better natural ventilation but it also increases the direct solar radiation penetration into indoor space, heat gain in summer and heat loss in winter. On the other hand, the ventilation rates decreasing problem with smaller window openings could be occurred. As a solution for it, the use of casement window can cause increasing natural ventilation rates by wing wall effect. This paper focuses on deduce the most efficient opening type of casement window in Korean climate. To estimate ventilation performance of each opening types, CFD simulation was used. The best performance of opening type in every wind direction is opening both windows to the center and the most appropriate opening type for Korean climate is also opening both windows to center.

Incorporating Genetic Algorithms into the Generation of Artificial Accelerations (인공 지진파 작성을 위한 유전자 알고리즘의 적용)

  • Park, Hyung-Ghee;Chung, Hyun-Kyo
    • Journal of the Earthquake Engineering Society of Korea
    • /
    • v.11 no.2 s.54
    • /
    • pp.1-9
    • /
    • 2007
  • The method of generating the artificial acceleration time histories for seismic analysis based on genetic algorithms is presented. For applying to the genetic algorithms, the frequencies are selected as the decision variables eventually to be genes. An arithmetic average crossover operator and an arithmetic ratio mutation operator are suggested in this study. These operators as well as the typical simple crossover operator are utilized in generating the artificial acceleration time histories corresponding to the specified design response spectrum. Also these generated artificial time histories are checked whether their outward features are to be coincident with the recorded earthquake motion or not. The features include envelope shape, correlation condition between 2 horizontal components of motion, and the relationship of max. acceleration, max. velocity and max. displacement of ground.

On the Chemical Evolution of Collapsing Starless Cores

  • Seo, Young-Min;Lee, Jeong-Eun;Kim, Jong-Soo;Hong, Seung-Soo
    • The Bulletin of The Korean Astronomical Society
    • /
    • v.35 no.2
    • /
    • pp.73.2-73.2
    • /
    • 2010
  • In order to understand internal dynamics of starless cores, molecular line emissions are usually observed. From profiles of the molecular lines, internal motions of starless cores have been deduced using a simple radiative transfer model such as the two-layer model (Myers et al.1996). This brings complexities arising from the chemical evolution. The motivation of this study is to follow the chemical evolution of a starless core that goes through gravitational contraction. For this purpose, we have performed hydrodynamical simulations with a marginally unstable Bonnor-Ebert sphere as an initial condition. We follow the chemical evolution of this core with changing conditions such as the chemical reaction rate at the dust surface and the strength of radiation field that penetrate into the core. At the core center, the molecules suffer from a higher degree of molecular depletion on the dust covered by ice rather than on the bare silicate dust. The stronger radiation field dissociates more molecules at the core envelope. From analysis on the line profile using the two-layer model, we found that the speed of inward motion deduced from the HCN F = 2-1 line adequately traces the true infall speed, when the dust is covered by ice and the core is exposed to the diffuse interstellar radiation field. Under different conditions, the two-layer model significantly underestimate the infall speed.

  • PDF

A Study on The Architectural Plan Access Method for The Integrated Design of The Environmentally Friendly Architecture (친환경 건축의 통합설계를 위한 건축 계획적 접근방법에 관한 연구)

  • Cho, Sung-Hyun;Kim, Chul-Kyu
    • Journal of The Korean Digital Architecture Interior Association
    • /
    • v.10 no.3
    • /
    • pp.79-86
    • /
    • 2010
  • From the research which sees the building which uses a natural control method with ecological architecture, continuity tried to divide the building which uses a physical control method with sustainable architecture. Ecological architecture analyzes the microclimate of the area and applies mining and natural ventilation leads and that the interior environment controls, the condition of the site actively and there is a possibility of seeing. Also sustainable architecture which is possible to lead and recycling and reuse of the resources and energy cyclic process of the construction resources to lead and the interior environment to control. Therefore the case where the facility system and structural system become integrated design organically in natural circulating method is many. Specially the sunshade system and double skin system are combined and structural system of the building and there is a possibility of having the envelope which form is feature. Today the buildings lead and the system integration process where the integral parts are systematic is demanded the interior environment which and an external form and that, they make they are there is a possibility of seeing. the environmental building which hits joins in with natural control method and the structure and facility system are integrated and has the tendency which is developed and there is a possibility of saying that a meaning with the alternative construction will be able to reduce the resources and an energy.

Flutter Analysis of F-16 Aircraft Using Test Modal Data (시험 모달 데이터를 이용한 F-16 항공기의 플러터 해석)

  • 변관화;전승문
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.34 no.4
    • /
    • pp.76-82
    • /
    • 2006
  • Flutter analyses are performed for the KF-16D aircraft with brand new ALQ-X ECM pod. A flutter analysis method using test modal data is proposed and validated using published F-16 modal data and flutter analysis results. Ground vibration test is performed for KF-16D stands on its landing gears. Attained modal data are transformed to free-free condition of KF-16D aircraft with ALQ-X pod and ALQ-119 pod, respectively. As the results of comparison of flutter analyses, ALQ-X is cleared to be operated in the flight envelope authorized for existing ECM pods.

Heating and Cooling Load according to the Climatic Conditions of Foreign Cities (해외 주요 도시의 기후특성에 따른 최대공조부하 요소별 분석)

  • An, Seung-Hyun;Kim, Jong-Ho;Lee, Jung-Hun;Lee, Sang-Yup;Song, Doo-Sam
    • Journal of the Korean Solar Energy Society
    • /
    • v.34 no.5
    • /
    • pp.81-87
    • /
    • 2014
  • According to the domestic construction business will continue stagnant, many domestic construction companies are expanding their business into foreign countries. As results, building design guidelines including HVAC design for foreign countries considering the regional climate conditions are needed. Also, green building design strategies to minimize the heating and cooling load are key issue to win a contract in construction business in the world. In this study, peak heating and cooling loads were calculated for the representative cities in the world : Seoul, St. Petersburg, Singapore and Mecca. The analyzed building was a typical high-rise office building and the building envelope properties, indoor heat gain, residence and operating schedules were same in all cases. Only the weather conditions were different by cases.