• Title/Summary/Keyword: Air attack

검색결과 251건 처리시간 0.031초

대기오염과 천식발작의 관련성에 관한 시계열적 연구 (Effect of Air Pollution on Emergency Room Visits for Asthma : a Time Series Analysis)

  • 주영수;조수헌
    • Journal of Preventive Medicine and Public Health
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    • 제34권1호
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    • pp.61-72
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    • 2001
  • Objectives : To evaluate the hypothesis that increasing ambient levels of ozone or particulate matter are associated with increased emergency room visits for asthma and to quantify the strength of association, if any, between these. Methods : Daily counts of emergency room visits for asthma, air quality, and weather data were collected from hospitals with over 200 beds and from monitoring Stations in Seoul, Korea from 1994 through 1997. Daily counts of emergency mom visits for asthma attack were analyzed using a general additive Poisson model, with adjustment for the effects of secular trend, seasonal variation, Sunday and holiday, temperature, and humidly, according to levels of ozone and particulate matter. Results : The association between daily counts of emergency room visits for asthma attack and ozone levels was statistically significant in summer(from June to August), and the RR by unit inclement of 100 ppb ozone was 1.30(95% CI = $1.11\sim1.52$) without lag time. With restriction of the period from April to September in 1996, the RR was 1.37(95% CI = $1.06\sim1.76$), and from June to August in 1995, the RR was 1.62(95% CI = $1.12\sim2.35$). In the data for children$(5\sim14yr)$, the RR was 2.57(95% CI = $1.31\sim5.05$) with restriction of the period from April to September in 1997. There was no Significant association between TSP levels and asthma attacks, but a slight association was seen between PM10 levels and asthma attacks in a very restricted period. Conclusion : There was a statistically significant association between ambient levels of ozone and daily counts of emergency room visits for asthma attack. Therefore, we must make efforts to effectively minimize air pollution, in order to protect public health.

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항공무기체계 사이버공격에 대한 작전영향성평가 프레임워크 제안 (Proposal of a framework for evaluating the operational impact of cyber attacks on aviation weapons systems(EOICA))

  • 홍병진;김완주;이수진;임재성
    • 융합보안논문지
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    • 제20권4호
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    • pp.35-45
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    • 2020
  • 최첨단 자산인 항공무기체계에 대한 사이버공격이 현실화되고 지속적인 위협으로 다가오고 있다. 그러나 현재 항공무기체계의 내장형 소프트웨어 특성상 평시 네트워크와 연결성 없이 관리되고 운용되어지고 있어 상대적으로 사이버공격에 대한 대응 관리가 취약한 실정이다. 따라서 사이버공격이 현실화 되었을 경우 그러한 공격이 항공임무명령서(ATO: Air Tasking Order) 수행에 미칠 악영향에 대한 평가방안과 대비가 절실하다. 본 논문에서는 항공무기체계에 대한 사이버공격이 발생할 경우 이에 대한 ATO수행의 혼란을 피하고 체계적인 대응을 위하여 작전영향성평가 프레임워크를 제안한다. 제안된 프레임워크는 항공무기체계 시스템별로 항공작전에 미치는 영향을 분석하고 이를 위한 대응조치들을 표준화함으로써 무경고하에 발생할 수 있는 사이버공격에 대하여 작전에 미치는 부정적 영향을 최소화할 수 있도록 설계되었다. 그리고 작전 지휘관이 사이버공격이 발생하는 상황 하에서도 작전수행을 위한 신속한 지휘결심을 할 수 있도록 지원한다.

흐름 영각에 따른 강제공랭 모듈 주위의 열전달 특성에 관한 연구 (A Study on the Heat Transfer Characteristics Around a Surface-Mounted Air-Cooled Module for the Flow Angle-of-Attack)

  • 박상희;신대종
    • 대한기계학회논문집B
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    • 제26권9호
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    • pp.1267-1275
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    • 2002
  • An experimental study was performed to investigate adiabatic wall temperature and heat transfer coefficient around a module cooled by forced air flow. The flow angle of attack to the module were 0$^{\circ}$and 45$^{\circ}$. In the first method, inlet air flow(1~7m/s) and input power.(3, 5, 7W) were varied after a heated module was placed on an adiabatic floor(320$\times$550$\times$1㎣). An adiabatic wall temperature was determinated to use liquid crystal film. In the second method to determinate heat transfer coefficient, inlet air flow(1~7m/s) and the heat flux of rubber heater(0.031~0.062W/$m^2$) were varied after an adiabatic module was placed on rubber heater covering up an adiabatic floor. Additional information is visualized by an oil-film method of the surface flow on the floor and the module. Plots of $T_{ad}$ and $h_{ad}$ show marked effects of flow development from the module and dispersion of thermal wake near the module. Certain key features of the data set obtained by this investigation may serve as a benchmark for thermal-design codes based on CFD.

Threats of MANPADS and Its Counter-Measures

  • Choi, Jin-Tai
    • International Journal of Contents
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    • 제6권3호
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    • pp.89-96
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    • 2010
  • The International air transportation industry provides a vital communication link which brings prosperity to many states in our modern age. This invaluable link has been threatened by terrorism. Airlines have been one of the most attractive targets in the eyes of terrorists for several reasons, including particularly the international and symbolic nature of aviation, and the potential of multigovernmental involvement which can inevitably generate wide publicity. Terrorist attacks against civil aviation have been committed since the earliest days of civil aviation history. The first attack against civil aircraft dates back to the early 1930s. Since then, aircraft hijacking and other forms of attack against air transport operations have become one of the most serious challenges to the safety of flying. In recent years, a new form of threats against civil aviation has appeared. Man-portable air defense systems (MANPADS) in the hands of criminals, terrorists, and other non-state actors pose a serious potential threat to passenger air travel, the commercial aviation industry, and military aircraft around the world. The purpose of this study is to provide some countermeasures against such attacks. In order to foster a better understanding of the problem, an introduction of MANPADS and a brief history of attacks using MANPADS are presented. It also examines the level of threats, trends of attacks using MANPADS and the possible countermeasures to be taken by the international community.

Missile Autopilot Design for Agile Turn Control During Boost-Phase

  • Ryu, Sun-Mee;Won, Dae-Yeon;Lee, Chang-Hun;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
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    • 제12권4호
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    • pp.365-370
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    • 2011
  • This paper presents the air-to-air missile autopilot design for a $180^{\circ}$ heading reversal maneuver during boost-phase. The missile's dynamics are linearized at a set of operating points for which angle of attack controllers are designed to cover an extended flight envelope. Then, angle of attack controllers are designed for this set of points, utilizing a pole-placement approach. The controllers' gains in the proposed configuration are computed from aerodynamic coefficients and design parameters in order to satisfy designer-chosen criteria. These design parameters are the closed-loop frequency, damping ratio, and time constant; these represent the characteristics of the control system. To cope with highly nonlinear and rapidly time varying dynamics during boost-phase, the global gain-scheduled controller is obtained by interpolating the controllers' gains over variations of the angle of attack, Mach number, and center of gravity. Simulation results show that the proposed autopilot design provides satisfactory performance and possesses good [ed: or "sufficient" or "excellent"] capabilities.

함정(공기부양정) 취약성 분석방법 연구 (The Study on the Methodology for Naval Ship(Craft Air Cushion) Vulnerability Analysis)

  • 최봉완;이찬선
    • 한국군사과학기술학회지
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    • 제13권6호
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    • pp.1106-1112
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    • 2010
  • One of the considerations in weapon systems procurement is the objective of maximizing the current force. Also, offensive effects, rather than defense are valued in weapons system development and procurement. Especially, the survivability of a naval ship is equally important as the offensive effect of onboard weapons. In case of naval ships, development of attack tactics and research regarding damage minimization must be conducted through live fire exercise against actual targets in order to minimize damage from the enemy. However, it is difficult to conduct such adequate measures due to realistic limitations such as time and budget in order to verify and calculate a weapon system's attack and damage effects along with the lack of practical studies in this subject despite numerous interests. Research are being conducted utilizing M&S to estimate attack effects and study damages due to such reason, but the lack of authoritative data and development ability are limiting calculation of reliable results. Therefore, this study will propose a measure to increase survivability of a weapon system(ship/vessel) utilizing research of vulnerability from enemy attacks analysis method against a naval ship(Craft Air Cushion).

모르터의 물리.화학적 특성에 미치는 중성화의 영향 (The Influence of Carbonation on Physical and Chemical Property in Mortar)

  • 문소현;소승영;소양섭
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1995년도 가을 학술발표회 논문집
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    • pp.30-34
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    • 1995
  • There are carbonatiion, salt attack, freezing & thawing and alkali-aggregate reactions as the cautions of durability lowering of concret structure. Generally, these cautions complicatedly lower the durability of structure and among these cautions the most serious problem is salt attack and carbonation. This study is intending to get the carbonation phenominon, that among cement calcium hydroxides change into calcium carbonate by responding to carbon mitrogen in the air.

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부순모래 콘크리트의 배합설계에 관한 실험적 연구 (An Experimental Study on the Mixing Design of the Concrete Using Crushed Sand)

  • 이진규;반호영;윤기원;최응규;한천구
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 1995년도 가을 학술발표회 논문집
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    • pp.35-40
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    • 1995
  • There are carbonatiion, salt attack, freezing & thawing and alkali-aggregate reactions as the cautions of durability lowering of concret structure. Generally, these cautions complicatedly lower the durability of structure and among these cautions the most serious problem is salt attack and carbonation. This study is intending to get the carbonation phenominon, that among cement calcium hydroxides change into calcium carbonate by responding to carbon mitrogen in the air.

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리브가 있는 판형 열교환기 관내부 최적화 (Optimization of the Channel of a Plate Heat Exchanger wits Ribs)

  • 이관수;양동근
    • 설비공학논문집
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    • 제14권3호
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    • pp.199-205
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    • 2002
  • In this paper, the optimum shape and arrangement of ribs in the channel of a plate heat exchanger are studied. The following dimensionless geometric parameters of ribs are selected as design variables: rib height ($H_R$), angle of attack ($\beta$), rib pitch ($P_R$), rib distance (L) and aspect ratio of rib (AR). The optimization is performed by minimizing the objective function consisting of the Nusselt number and the friction factor. The optimal values of design variables are as follows: $H_R$=0.263, $\beta$=0.290, $P_R$=3.142, L: 3.954, AR=0.342. The pressure drop and the heat transfer of the optimum model, compared to those of the reference model, are increased by 15.1% and 41.6%, respectively.

가설 검증과 칼만 필터를 이용한 격추평가 기법 연구 (A Kill-Assessment Technique Using Hypothesis Testing and Kalman Filter)

  • 김호정;이동관
    • 한국군사과학기술학회지
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    • 제9권4호
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    • pp.5-14
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    • 2006
  • The correct and opportune decision of reengaging the intercepted target is required in order to enhance the engagement performance of the surface to air missile systems that has the ability to defense or attack against various targets at the same time. The engagement efficiency and success of these systems will be largely enhanced by assigning quickly its system resources to the intercepted target and minimizing the waste of system resources for the target which is not able to attack any more. The kill-assessment algorithm has to be able to evaluate automatically whether various targets intercepted by missiles are killed or not on the basis of the reasonable confidence level. The definition of kill assessment is discussed and the kill assessment algorithm is designed reliably by using Kalman filter and a probability theory. Finally its performance is evaluated and analyzed by the Monte Carlo simulation.