• Title/Summary/Keyword: Fin systems

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Covariance analysis describing function technique for missile performance (CADET를 이용한 가로방향 힘의 Saturation에 대한 미사일의 성능해석)

  • 김진호
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10a
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    • pp.456-459
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    • 1993
  • CADET is used to analyze the performance of the missile. Miss distance is calculated for a given lateral fin force saturation level due to the aerodynamic characteristics, target acceleration, and glint and fading noises which is assumed as Gaussian noises. As .alpha.-.betha. filter is studied to attenuate the noises, the results are compared with those of without filter. For the easy simulation, the transfer function of a discrete .alpha.-.betha. filter is converted into the continuous model. Simulation results show that the results of CADET simulation is similar to those of Monte-Carlo simulation. Moreover CADET is the better in computing time demand.

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Experimental study on aerodynamic characteristics of launcher at subsonic speed (아음속 유동에서의 발사체의 공력특성에 관한 실험 연구)

  • 노오현;이동호;김원욱;김철완
    • 제어로봇시스템학회:학술대회논문집
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    • 1988.10a
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    • pp.608-613
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    • 1988
  • Subsonic aerodynamic force and moment characteristics have been determined for parametric groups of launchers. Geometric variables considered in the experimental study were body length, nose planform, fin planform (body-alone contained), number of stage and existence of extrnal booster, All data were obtained for angles of attack from 0 to 27 deg in 3-deg. increments.

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Command to line of sight guidance loop based on LQG design (LQG 설계에 의한 시선지령 유도루우프의 구성)

  • Chang, Sang-Keun;Lyou, Joon
    • 제어로봇시스템학회:학술대회논문집
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    • 1992.10a
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    • pp.567-571
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    • 1992
  • A guidance loop of the missile system which uses a command to line of sight(CLOS) guidance law is designed based on LQG theory. In the environment of the severe tracking system noise, the system requires small aerodynamic control fin travel and small miss distance simultaneously. Results from a sample airframe shows good performance against a randomly maneuvering target.

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Design of air-cooled waste heat removal system with string type direct contact heat exchanger and investigation of oil film instability

  • Moon, Jangsik;Jeong, Yong Hoon;Addad, Yacine
    • Nuclear Engineering and Technology
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    • v.52 no.4
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    • pp.734-741
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    • 2020
  • A new air-cooled waste heat removal system with a direct contact heat exchanger was designed for SMRs requiring 200 MW of waste heat removal. Conventional air-cooled systems use fin structure causing high thermal resistance; therefore, a large cooling tower is required. The new design replaces the fin structure with a vertical string type direct contact heat exchanger which has the most effective performance among tested heat exchangers in a previous study. The design results showed that the new system requires a cooling tower 50% smaller than that of the conventional system. However, droplet formation on a falling film along a string caused by Rayleigh-Plateau instability decreases heat removal performance of the new system. Analysis of Rayleigh-Plateau instability considering drag force on the falling film surface was developed. The analysis results showed that the instability can be prevented by providing thick string. The instability is prevented when the string radius exceeds the capillary length of liquid by a factor of 0.257 under stagnant air and 0.260 under 5 m/s air velocity.

Histology and Morphometries of the Epidermis of the Fins and Sucking Disc of the Mudskipper, Periophthalmus modestus (Pisces, Gobiidae)

  • Park, Jong-Young;Kim, Ik-Soo;Lee, Yong-Joo;Kim, So-Young
    • Animal cells and systems
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    • v.8 no.2
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    • pp.111-115
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    • 2004
  • The epidermis of the mudskipper, Periophthalmus modestus, consists of three layers- the outermost layer, middle layer and stratum germinativum. Extensive fine blood capillaries are present near the superficial layer of epidermis and outermost layer in five fins and a sucking disc. The diffusion distance between the vascular capillaries and the surface of epidermis ranged from 3.6 to 10.9${\mu}$m: 3.6 ${\mu}$m in the sucking disc, 10.9 ${\mu}$m in the anal fin and 4.6 to 5.0 ${\mu}$m in the two dorsal fins. Rate of the surface area of respiratory epithelium, the surface area of the fine blood capillaries occupied per surface area of epidermis in 0.1mm, is 3.7 to 4.4% in two dorsal fins and 1.1% in the anal fin. The middle layer is simpler in structure consisting of small or voluminous cells swollen by epidermal cells, and this layer appeared web-like. Well-developed lymphatic spaces containing lymphocytes existed in the stratum germinativum. The five fins and sucking disc had no epidermal glands.

Theoretical Analysis on Heat Transfer Characteristics and Heat Flux Performance in Ondol Systems of Dried Type (건식온돌시스템의 전열특성 및 방열성능에 관한 이론적 분석)

  • Jang, Yong-Sung;Yu, Ki-Hyung;Cho, Dong-Woo
    • Proceedings of the SAREK Conference
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    • 2007.11a
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    • pp.176-181
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    • 2007
  • This study aims to evaluate theoretically heat transfer characteristics and heat flux performance in ondol system of dried type is composed of panel of ceramics to improve of thermal conductivity and fin to expand heat. To this end, we analyzed effect of design factors(temperature of hot water, set temperature of room and thermal conductivity of finishing materials) in ondol system of dried type by heat transfer analysis. The main results of this study are summarized as follows; The deviation of heat flux and temperature was reduced by heat expansion from fin decreasing heat loss generated in air layer. The temperature and heat flux in upper finishing materials surface linearly increased according to temperature increment of hot water, but the temperature distribution in upper surface was assessed uneven. The greater heat resistance value of upper finishing materials, the deviation of maximum temperature and minimum temperature was decreased. Also, we suggested a basic design data about ondol system of dried type through an analysis of simulation results on heat transfer characteristics and heat flux performance.

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A Development of Counter Flow Type of Cooling System for Effective Panel Cooling (효과적인 패널 냉각을 위한 대향류형 냉각장치의 개발)

  • Lee, Joong-Soon
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.11 no.3
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    • pp.802-807
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    • 2010
  • The high efficient and cooling system is very important to the control panels of electrical distributors, and Industrial automated system including computer. Also, it can be used widely in various industrial systems such as industrial robots, numerically controlled machining center, and so on. The cooling method which flowing gasses were forced to circulate by compulsion was adapted in this study. then development of counter flow type of cooling system for effective panel cooling. In the present study, fin assembly was developed for this cooling system. As results, the developed system has the improvements of cooling performances and radiant heat ratio. Its increasing of airflow mass is about 20%, and radiation rate of heating is twice or more as high as the conventional system.

Numerical Model Development of a Microchannel Condenser for Mobile Air-Conditioning Systems (자동차용 에어컨의 마이크로채널 응축기의 수치적 모델 개발)

  • ISHAQUE, SHEHRYAR;ULLAH, NAVEED;CHOI, JUN-HO;KIM, MAN-HOE
    • Transactions of the Korean hydrogen and new energy society
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    • v.33 no.4
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    • pp.430-436
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    • 2022
  • This paper presents the numerical model development of a microchannel heat exchanger in mobile air-conditioning and heat pump applications. The model has been developed based on the effectiveness-NTU method using a segment-by-segment modeling approach. State-of-art correlations are used for refrigerant- and air-side heat transfer coefficients and pressure drops. The calculated heat condenser capacities are in good agreement with experimental data, with an average difference of 1.86%. The current model can be used for microchannel condenser simulations under various operating conditions. It is anticipated to improve productivity in designing and optimizing microchannel heat exchangers with folded louver fin geometry.

Automated measurement and analysis of sidewall roughness using three-dimensional atomic force microscopy

  • Su‑Been Yoo;Seong‑Hun Yun;Ah‑Jin Jo;Sang‑Joon Cho;Haneol Cho;Jun‑Ho Lee;Byoung‑Woon Ahn
    • Applied Microscopy
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    • v.52
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    • pp.1.1-1.8
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    • 2022
  • As semiconductor device architecture develops, from planar field-effect transistors (FET) to FinFET and gate-all-around (GAA), there is an increased need to measure 3D structure sidewalls precisely. Here, we present a 3-Dimensional Atomic Force Microscope (3D-AFM), a powerful 3D metrology tool to measure the sidewall roughness (SWR) of vertical and undercut structures. First, we measured three different dies repeatedly to calculate reproducibility in die level. Reproducible results were derived with a relative standard deviation under 2%. Second, we measured 13 different dies, including the center and edge of the wafer, to analyze SWR distribution in wafer level and reliable results were measured. All analysis was performed using a novel algorithm, including auto fattening, sidewall detection, and SWR calculation. In addition, SWR automatic analysis software was implemented to reduce analysis time and to provide standard analysis. The results suggest that our 3D-AFM, based on the tilted Z scanner, will enable an advanced methodology for automated 3D measurement and analysis.

The effect of heat exchanger type for exhaust heat recovery system on diesel engine performance (배기 열 회수 열교환기 형식이 디젤 엔진 성능에 미치는 영향)

  • Kim, Cheol-Jeong;Choi, Byung-Chul;Park, Kweon-Ha
    • Journal of Advanced Marine Engineering and Technology
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    • v.38 no.6
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    • pp.639-647
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    • 2014
  • Due to global warming and depletion of fossil fuels, technologies reducing $CO_2$ emission and increasing fuel efficiency simultaneously are required. An exhaust gas heat recovery system is a technology to satisfy both issues. This study analyses three types of heat exchanger installed on an exhaust pipe. In case of plate type heat exchanger, back pressure rapidly increased and maximum cylinder pressure reduced in high speed and maximum load, and back pressure increased over twice and specific fuel consumption also increased up to 2% which were the highest increasing rate. In case of fin tube type, the amounts of exhaust emissions and specific fuel consumption rate were less than the other two types. The effect of shell and tube was in the middle. Making a decision by only the effect on engine performance, a fin tube type is the best for exhaust heat recovery systems.