• Journal of Mechanical Science and Technology
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• 제20권1호
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• pp.167-175
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• 2006

A parametric study has been accomplished to figure out the effects of elliptic cylinder thickness, angle of attack, and Reynolds number on the unsteady lift and drag forces exerted on the elliptic cylinder. A two-dimensional incompressible Navier-Stokes flow solver is developed based on the SIMPLER method in the body-intrinsic coordinates system to analyze the unsteady viscous flow over elliptic cylinder. Thickness-to-chord ratios of 0.2, 0.4, and 0.6 elliptic cylinders are simulated at different Reynolds numbers of 400 and 600, and angles of attack of $10^{\circ},\;20^{\circ},\;and\;30^{\circ}$. Through this study, it is observed that the elliptic cylinder thickness, angle of attack, and Reynolds number are very important parameters to decide the lift and drag forces. All these parameters also affect significantly the frequencies of the unsteady force oscillations.

• 한국전산유체공학회지
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• 제13권2호
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• pp.1-7
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• 2008

For Aerodynamic analysis of vehicle at altitude, 100km, the validity of governing equations based on continuum model, was reviewed. Also, as the preliminary study for the sub-orbital space plane development, a candidate geometry was suggested and computational fluid dynamic(CFD) analysis was performed for various angles of attack in subsonic and supersonic flow regimes to analyze the aerodynamic characteristics and performance. The inviscid flow analyses showed that the stall starts at angle of attack above $20^{\circ}$, the maximum drag is generated at angle of attack, $87^{\circ}$ and the maximum lift to drag ratio is about 8 in subsonic flow. In supersonic, the stall angle is about $40^{\circ}$ and the maximum drag is generated at angle of attack, $90^{\circ}$. Also, mach number distribution of re-entry vehicle was computed versus altitudes.

• Journal of Mechanical Science and Technology
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• 제18권6호
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• pp.1042-1051
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• 2004

The vortex flow characteristics of a sharp-edged delta wing at high angles of attack were studied using a computational technique. Three dimensional, compressible Reynolds-averaged Navier-Stokes equations were solved to understand the effects of the angle of yaw, angle of attack, and free stream velocity on the development and interaction of vortices and the relationship between suction pressure distributions and vortex flow characteristics. The present computations gave qualitatively reasonable predictions of vortical flows over a delta wing, compared with past wind tunnel measurements. With an increase in the angle of yaw, the symmetry of the pair of leading edge vortices was broken and the vortex strength was decreased on both windward and leeward sides. An increase in the free stream velocity resulted in stronger leading edge vortices with an outboard movement.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.45-49
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• 2007

Asymmetric force and vibration caused by separation flow at high angle of attack affect the stability of supersonic missile. As a preliminary study we verified the effect of turbulence model through general 3-D slender body for the supersonic flow at high angle of attack. ${\kappa}-{\omega}$ Wilcox model, ${\kappa}-{\omega}$ Wilcox-Durbin+ model, ${\kappa}-{\omega}$ shear-stress transport model, and Spalart-Allmaras one equation model are used. Grid sensitivity test was performed with three different grid system. results show that all models are in good agreement with the experimental data.

• 스마트미디어저널
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• 제4권4호
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• pp.24-32
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• 2015

최근 SDN은 데이터센터 네트워크로 활발히 사용되고 있으며, 그 사용범위를 점진적으로 늘려나가고 있다. 이러한 새로운 네트워크 환경 변화와 함께, 네트워크 보안시스템을 SDN 환경 상에서 구축하는 연구들이 진행되고 있다. 특히 OpenFlow Switch의 포트를 통과하는 패킷들을 지속적으로 관찰함으로써 네트워크 플러딩 공격 등을 탐지하기 위한 시스템들이 제안되었다. 하지만 다수의 스위치를 중앙집중형 컨트롤러에서 관리하는 SDN의 특성상 지속적인 네트워크 트래픽 관찰은 상당한 오버헤드로 작용할 수 있다. 이 논문에서는 이러한 지속적인 네트워크 트래픽 관찰에 따른 오버헤드를 줄이면서도 네트워크 플러딩 공격을 효과적으로 탐지 및 방어 할 수 있는, 샘플링 기반 네트워크 플러딩 공격 탐지 및 방어 시스템을 제안한다. 제안된 시스템은 네트워크 트래픽을 주어진 샘플링 조건에 맞추어 주기적으로 관찰하고, 샘플링 패킷들을 분석하여 네트워크 플러딩 공격을 탐지하며, 탐지된 공격을 OpenFlow Switch의 플로우 엔트리관리를 통해 능동적으로 차단하다. 네트워크 트래픽 샘플링을 위해 sFlow agent를 활용하고, 샘플링된 패킷 정보를 소프트웨어적으로 분석하여 공격을 탐지하기 위해 오픈소스 기반 IDS인 snort을 사용하였다. 탐지된 공격의 자동화된 방어 기작의 구현을 위해 OpenDaylight SDN 컨트롤러용 어플리케이션을 개발하여 적용하였다. 제안된 시스템은 OVS (Open Virtual Switch)를 활용한 로컬 테스트베드 상에서 그 동작을 검증하였고, 다양한 샘플링 조건에 따른 제안된 시스템의 성능 및 오버헤드를 분석하였다.

• International Journal of Aeronautical and Space Sciences
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• 제14권3호
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• pp.201-209
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• 2013

Much numerical and experimental research has been done for the flow around an oscillating airfoil. The main research topics are vortex shedding, dynamic stall phenomenon, MAV's lift and thrust generation. Until now, researches mainly have been concentrated on analyzing the wake flow for the variation of frequency and amplitude at a low angle of attack. In this study, wake structures and acoustic wave propagation characteristics were studied for a plunging airfoil at high angle of attack. The governing equations are the Navier-Stokes equation with LES turbulence model. OHOC (Optimized High-Order Compact) scheme and 4th order Runge-Kutta method were used. The Mach number is 0.3, the Reynolds number is, and the angle of attack is from $20^{\circ}$ to $50^{\circ}$. The plunging frequency and the amplitude are from 0.05 to 0.15, and from 0.1 to 0.2, respectively. Due to the high resolution numerical method, wake vortex shedding and pressure wave propagation process, as well as the propagation characteristics of acoustic waves can be simulated. The results of frequency analysis show that the flow has the mixed characteristics of the forced plunging frequency and the vortex shedding frequency at high angle of attack.

• 전기학회논문지
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• 제65권12호
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• pp.2240-2250
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• 2016

MIFARE Classic is the most popular contactless smart card, which is primarily used in the management of access control and public transport payment systems. It has several security features such as the proprietary stream cipher Crypto 1, a challenge-response mutual authentication protocol, and a random number generator. Unfortunately, multiple studies have reported structural flaws in its security features. Furthermore, various attack methods that target genuine MIFARE Classic cards or readers have been proposed to crack the card. From a practical perspective, these attacks can be partitioned according to the attacker's ability. However, this measure is insufficient to determine the optimal attack flow due to the refined random number generator. Most card-only attack methods assume a predicted or fixed random number, whereas several commercial cards use unpredictable and unfixable random numbers. In this paper, we propose optimal MIFARE Classic attack procedures with regards to the type of random number generator, as well as an adversary's ability. In addition, we show actual attack results from our portable experimental setup, which is comprised of a commercially developed attack device, a smartphone, and our own application retrieving secret data and sector key.

• 대한기계학회논문집
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• 제15권6호
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• pp.1919-1932
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• 1991

본 연구에서는 고강도 알루미늄 합금으로 제작된 평판보의 받음각(.alpha.)를 10˚ 에서 30˚까지 10˚씩 변화시킨 3가지의 모델에 대해, 각 모델의 Re$_{d}$수 변화에 대한 후류의 스펙트럼분석, 레이저 도플러 유속계(laser doppler velocimetry)를 이용 한 유동장 해석 및 평판보의 응답을 실험을 통해 조사, 분석하고 유동장과 측정이 용 이하지 않은 얇은 평판주위의 압력분포에 대한 전산해석을 수행함으로써 유동 여기진 동 구조의 규명을 시도하였다.다.

• 정보처리학회논문지C
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• 제13C권4호
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• pp.397-404
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• 2006

소프트웨어 공격이 성공하기 위해서는 공격 코드가 프로그램의 주소 공간에 주입된 후 프로그램의 제어 흐름이 공격 코드 위치로 변경되어야 한다. 프로그램의 주소 공간 중 코드 영역은 실행 중에 변경이 불가능하므로 공격 코드가 주입될 수 있는 곳은 데이터 영역 밖에 없다. 따라서 데이터 영역으로 프로그램의 제어가 변경될 경우 주입된 공격 코드로 제어가 옮겨 가는 공격이 발생한 것으로 판단할 수 있다. 따라서 본 논문에서는 프로그램의 제어 흐름과 관련된 CALL, JMP, RET 명령어의 목적 주소를 검사하여 제어가 옮겨갈 목적 주소가 프로그램의 실행 코드가 저장된 텍스트 영역이 아닌 데이터 영역일 경우 소프트웨어 공격이 발생한 것으로 간주하는 소프트웨어 공격 탐지 기법을 제안하였다. 제안된 방법을 이용하면 함수의 복귀주소뿐만 아니라 함수포인터, longjmp() 버퍼 등 프로그램 제어 흐름과 관련된 모든 데이터가 변경되었는지 점검할 수 있었기 때문에 기존 기법들보다 더 많은 종류의 공격을 탐지할 수 있었다.

• 대한기계학회논문집B
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• 제22권4호
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• pp.530-541
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• 1998

Heat transfer augmentation in a rib-roughened duct is affected by the rib configurations, such as rib height, angle of attack, shape, rib to rib pitch, and aspect ratio of a duct. These have been the main subjects in studying the average heat transfer and the friction loss of the fully developed flow. Investigating distributions of local heat transfer coefficients and flow patterns in a duct with the rib turbulators is necessary to find the characteristics of heat transfer augmentation and to decide the optimal configurations of ribs. In the present study the numerical analyses and the mass transfer experiments are performed to understand the flow through a rib roughened duct and the heat transfer characteristics with various angles of attack of ribs. A pair of counter-rotating secondary flow in a duct has a main effect on the lateral distributions of local mass transfer coefficients. Downwash of the rotating secondary flow, reattachment of main flow between ribs and the vortices near ribs and wall enhanced the mass transfer locally up to 8 times of that in case of the duct without ribs.