• Title/Summary/Keyword: Attack Model

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DESIGN-ORIENTED AERODYNAMIC ANALYSES OF HELICOPTER ROTOR IN HOVER (정지비행 헬리콥터 로터의 설계를 위한 공력해석)

  • Jung H.J.;Kim T.S.;Son C.H.;Joh C.Y.
    • Journal of computational fluids engineering
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    • v.11 no.3 s.34
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    • pp.1-7
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    • 2006
  • Euler and Navier-Stokes flow analyses for helicopter rotor in hover were performed as low and high fidelity analysis models respectively for the future multidisciplinary design optimization(MDO). These design-oriented analyses possess several attributes such as variable complexity, sensitivity-computation capability and modularity which analysis models involved in MDO are recommended to provide with. To realize PC-based analyses for both fidelity models, reduction of flow domain was made by appling farfield boundary condition based on 3-dimensional point sink with simple momentum theory and also periodic boundary condition in the azimuthal direction. Correlations of thrust, torque and their sensitivities between low and high complexity models were tried to evaluate the applicability of these analysis models in MDO process. It was found that the low-fidelity Euler analysis model predicted inaccurate sensitivity derivatives at relatively high angle of attack.

Optimal deployment strategy of patriot missile (패트리어트 (patriot) 미사일의 최적 배치)

  • 김영휘;김성인;오원민
    • Proceedings of the Korean Operations and Management Science Society Conference
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    • 1994.04a
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    • pp.29-37
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    • 1994
  • It is reported that north Korea has already developed 1,500 to 2,000-km-range Scud missile. As a defensive strategy against Scud attack on military and civilian facilities the military authorities are considering deployment of Patriot missile. This paper deals with its optimal deployment strategy. In this problem a Patriot missile which has multiple-facility responsibility may be able to protect each of its assigned facilities only with a certain probability, not absolute protection, and it may not be adequate to have only a single missile protect a facility, either because of its operational reliability or because of its limited availability at any given point in time. We formulate this problem into the probabilistic partial set covering model developed by Sherali and Kim. The applicability, verification and validation of the model are tested via an abbreviated case study.

Linear controller design for the longitudinal model of a reusable launch vehicle X-33

  • Woo, Young-Tae;Kim, Jae-Jin;Kim, Young-Chol
    • 제어로봇시스템학회:학술대회논문집
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    • 2005.06a
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    • pp.1978-1982
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    • 2005
  • In this paper, a linear controller is designed for the longitudinal model of X-33 in TAEM (The Terminal Area Energy Management) phase. The CRA (Characteristic Ratio Assignment) is used as the continuous time design method such that the output response of X-33 control system tracks the reference command. The performance of the proposed controller is evaluated through the step response. Also simulation results show that the initial state of the plant is dominantly affected by the poles and zeros of the plant.

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Development of Early Evaluation System for Concrete Quality, Construction and Maintenance (콘크리트 품질ㆍ시공ㆍ유지관리의 조기판정시스템 개발)

  • 손용우;이증빈;최미라;박봉수
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2004.10a
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    • pp.517-526
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    • 2004
  • In the resent years, the early evaluation of concrete quality, construction and maintenance has been considered as all is of major concern due to the increase of loading and the degradation of structures related with time. This paper presents evaluation of structural safety performance using measured data of construction, on the basis of a field measurements for the prevention of unreliable concrete works. Measurements analyzed in this paper are early quality condition and performance assessment, serviceability performance by cracks and deflection, rating performance by loading, durability performance by chloride attack and carbonation. Thus, a quantitative assessment model of resistance capacity was developed here to meet the requirement for deteriorated concrete structures. The model focuses on damage mechanical of concrete structures deteriorated by initial damage factors for concrete quality and environment factors such as chloride and carbonation attacks. These results could provide useful information for concrete structures interested in design, construction and maintenance.

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Can the Point Defect Model Explain the Influence of Temperature and Anion Size on Pitting of Stainless Steels

  • Blackwood, Daniel J.
    • Corrosion Science and Technology
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    • v.14 no.6
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    • pp.253-260
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    • 2015
  • The pitting behaviours of 304L and 316L stainless steels were investigated at $3^{\circ}C$ to $90^{\circ}C$ in 1 M solutions of NaCl, NaBr and NaI by potentiodynamic polarization. The temperature dependences of the pitting potential varied according to the anion, being near linear in bromide but exponential in chloride. As a result, at low temperatures grades 304L and 316L steel are most susceptible to pitting by bromide ions, while at high temperatures both stainless steels were more susceptible to pitting by small chloride anions than the larger bromide and iodide. Thus, increasing temperature appears to favour attack by smaller anions. This paper will attempt to rationalise both of the above findings in terms of the point defect model. Initial findings are that qualitatively this approach can be reasonably successful, but not at the quantitative level, possibly due to insufficient data on the mechanical properties of thin passive films.

Management System for Saemangeum Gate Bridge (배수갑문 교량의 노후도 감시시스템)

  • Lee, Joon-Gu;Cho, Young-Kwon;Kim, Han-Joung;Kim, Kwan-Ho;Kim, Myung-Won
    • Proceedings of the Korea Concrete Institute Conference
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    • 2006.05b
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    • pp.241-244
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    • 2006
  • The basic prediction model was constructed to obtain optimal maintenance method for concrete structure under marine environment by exploring the mechanism of mono and combined deterioration in lab. This model was planned to be upgraded with data acquired from several exposure specimens under same environment as structures. The computer program developed to give useful guidance observer would be improved. Several repair materials and repair construction methods applied to exposure specimens will be tested for its performance of prohibit salt attack and freezing & thawing action during experimental period about ten years. All of these data could be available to complete the prediction system. The manager will be able to use the system for optimal maintenance of marine concrete structures.

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Prediction System of Deterioration Ratio for Marine Concrete Structures (해양콘크리트 구조물의 노후도 예측시스템 개발 연구)

  • Lee, Joon-Gu;Park, Kwang-Su;Cho, Young-Kwon;Lee, Chang-Su;Kim, Han-Joung
    • Proceedings of the Korea Concrete Institute Conference
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    • 2005.11a
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    • pp.531-534
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    • 2005
  • The basic prediction model was constructed to obtain optimal maintenance method for concrete structure under marine environment by exploring the mechanism of mono and combined deterioration in lab. This model was planned to be upgraded with data acquired from several exposure specimens under same environment as structures. The computer program developed to give useful guidance observer would be improved. Several repair materials and repair construction methods applied to exposure specimens will be tested for its performance of prohibit salt attack and freezing & thawing action during experimental period about ten years. All of these data could be available to complete the prediction system. The manager will be able to use the system for optimal maintenance of marine concrete structures.

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PREDICTION OF AERODYNAMIC CHARACTERISTICS AND BODY VORTICES OVER SUPERSONIC MISSILES (초음속 유도탄의 동체 와류 예측 및 공력 특성 분석)

  • Yoon, S.H.;Kim, Chang-Am;Hur, K.H.
    • 한국전산유체공학회:학술대회논문집
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    • 2010.05a
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    • pp.308-314
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    • 2010
  • In this study, NASA test model with four cruciform fins is utilized to validate the in-house code. Sur face pressure distribution and aerodynamic coefficients are compared with experimental data. Through extensive validation work, it is verified that the code has capability to predict aerodynamic characteristics of missile configuration. In inviscid analysis through a relatively low computational time, analysis result close to experimental data can be confirmed. However, at high angle of attack more than 20 degree, the accuracy of analysis is gradually decreased due to massive separation. In addition, it has been seen that Reynolds number, turbulence model and numerical method have effects on body vortices and aerodynamic characteristics.

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Improvement of Paraglider by Using Axiomatic Approach (공리적 접근법을 이용한 패러글라이더 성능 개선에 관한 연구)

  • 류상우;차성운;임웅섭
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2001.04a
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    • pp.719-722
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    • 2001
  • Paraglider has been used for a good air sports instrument by many people in the world though its short history. And manufacturers have improved it continuously. It has the great growth from the first model like parachute to the latest model that has the extreme speed, but we can improve it in more parts. In this paper, we will show the method which can improve its performance by using Axiomatic Approach.

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A Study on the Vortex Generators of Plastic Plate Heat Exchangers (플라스틱 판형 열교환기의 와류발생기에 관한 연구)

  • Oh Yunyoung;Yoo Seongyeon;Ko Sungho
    • Proceedings of the KSME Conference
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    • 2002.08a
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    • pp.107-110
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    • 2002
  • The present study deals with CFD analysis of 'The vortex generators on plastic plate heat exchanger'. When a vortex generator is placed on the heat transfer surface, the flow gets more complex because it entails complicated three-dimensional flows such as separation, reattachment, and recirculation. CFX-5.4, a commercial code utilizing unstructured mesh, has been used as a computational method for solving RANS(Reynolds-Averaged Wavier-Stokes) equations, and the applied turbulence model is $k-{\varepsilon}$ model. In addition, those computational analyses were implemented under various conditions , with or without the vortex generator between two plates, the number, form and the size of vortex generator, and different attack of angle. From the calculated temperature, velocity and pressure distribution, vorticity, wall heat flux and so on under those conditions, this study shows the effect of vortex on heat transfer.

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