• 한국군사과학기술학회지
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• 제17권4호
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• pp.551-559
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• 2014

The influence of the battle damage hole on the velocity and vorticity flow field have been studied by using particle image velocimetry. Time averaged velocity and vorticity vector fields in the vicinity of jet are presented. The perforated damage hole on a wing created from a hit by anti-air artillery was modeled as a 10% chord size hole which positioned at quarter chord. At low angles of attack, the vorticity in the forward side of the jet is cancelled due to mixing with the wing surface boundary layer. Stretching of vorticity in the backside of the jet generates a semi-cylindrical vortical layer that enclosing a domain with slow moving reverse flow. Conversely, at higher the angles of attack, the jet vorticity advected away from the wing surface and remains mostly confined to the jet. The mean flow behind the jet has a wake-like structure.

• 한국기계가공학회지
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• 제18권8호
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• pp.51-59
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• 2019

Flow forming is an eco-friendly and high-efficiency plastic deformation process with fewer chips during a process which is specifically used to manufacture seamless tubular products like tire wheels, rocket motor cases etc. On the development of mortar barrel using Inconel718 tube, some flow formed products had dimensional errors on their thickness. In this study, our purpose is to optimize the process conditions with the smallest dimensional error. In order to find an optimum process condition, 2D axisymmetric FEM simulation analyses with Taguchi method were conducted. Geometric variables (attack angle, flatting angle, roller nose radius) and operating parameters (depth of forming, feed rate) are considered as control factors. Forward flow forming with single roller was first analyzed to determine the effective factors using AFDEX software and attack angle of the roller was identified as the most influential factor. Also, the nose radius of the rollers was confirmed as a significant factor in multi-rollers flow forming system. The effect of rollers offset values are also studied and finally, we proposed optimal conditions to improve the accuracy of flow forming process with Inconel718 tube for mortar barrel manufacturing.

• 한국컴퓨터정보학회논문지
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• 제10권2호
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• pp.39-47
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• 2005

본 논문에서는 전송되는 메시지의 무결성과 출처 인증을 위해 광범위하게 사용되는 메시지 인증 코드 (Message Authentication Code :MAC) 알고리즘을 제안하고 안전성을 분석한다. 제안된 MAC 알고리즘은 기본 블록 암호로 64-비트 블록과 56-비트 키를 가진 64비트 블록 암호 알고리즘을 이용하여 MAC 값의 길이를 64-비트와 32-비트를 사용하였을 경우의 안전성을 비교한다. 또한, 128-비트 블록과 128-비트 키를 가진 128비트 블록 암호 알고리즘을 이용하여, MAC 값의 길이를 128비트와 64-비트를 사용하였을 경우의 안전성을 비교한다 그래서 메시지의 길이와 MAC값의 길이에 따른 위장 공격의 안전성을 분석한다.

• 한국태양에너지학회 논문집
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• 제35권4호
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• pp.43-55
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• 2015

This paper presents the thermal hydraulic performance of a three dimensional rib-roughened solar air heater (SAH) duct with the one principal wall subjected to uniform heat flux. The SAH duct has aspect ratio of 12.0 and the Reynolds number ranges from 2000 to 12000. The roughness has relative rib height of 0.045, ratio of dimple depth to print diameter of 0.5 and rib pitch ratio of 8.0. The flow attack angle is varied from $35^{\circ}$ to $70^{\circ}$. Various turbulent flow models are used for the heat transfer and fluid flow analysis and their results are compared with the experimental results for smooth surfaces. The computational fluid dynamics (CFD) results based on the renormalization k-epsilon model are in better outcomes compared with the experimental data. This model is used to calculate heat transfer and fluid flow in SAH duct with the compound roughness of V-shaped ribs and dimples. The overall thermal performance based on equal pumping power is found to be the highest (2.18) for flow attack angle of $55^{\circ}$. The thermo-hydraulic performance for V-pattern shaped ribs combined with dimple ribs is higher than that for dimple rib shape and V-pattern rib shape air duct.

• Journal of Advanced Marine Engineering and Technology
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• 제26권4호
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• pp.485-492
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• 2002

The present study is aimed to reveal macroscopic aerodynamic characteristics of two-dimensional rectangular prisms with three aspect ratios(D/H=1, 2 and 3) and six angles of attack($0^{circ}, 10^{circ}, 13.5^{circ}, 20^{circ}, 30^{circ} and 45^{\circ}$). The Reynolds number is fixed as $1\times10^4$. The SOLA-based revised finite difference method for the conservation form on irregular grid was adopted as a new numerical method. Instantaneous flow patterns at $45^{\circ}$ in case of D/H=2 and D/H=3 show larger asymmetric wake development which is closely related to the sharp decrease of drag coefficients at higher angles of attack range. Vorticity propagation into enlarged wake region is conjectured to be responsible for this phenomenon. The Strouhal number is found to be sensitive to the angle of attack at higher aspect ratios(D/H=2 and 3).

• 디지털산업정보학회논문지
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• 제6권3호
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• pp.31-36
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• 2010

In this paper, We propose a transaction signing-based authentication scheme for protecting sinkhole attacks in wireless sensor networks. Sinkhole attack makes packets that flow network pass through attacker. So, Sinkhole attack can be extended to various kind of attacks such as denial of service attacks, selective delivery or data tamper etc. We analyze sinkhole attack methods in directed diffusion based wireless sensor networks. For the purpose of response to attack method, Transaction signing-based authentication scheme is proposed. This scheme can work for those sensor networks which use directed diffusion based wireless sensor networks. The validity of proposed scheme is provided by BAN logic.

• 한국어업기술학회:학술대회논문집
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• 한국어업기술학회 2005년도 춘계 학술대회 논문집
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• pp.62-69
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• 2005

Maneuverability of ships has been receiving a great deal of attention both concerning navigation safety and the prediction of ship maneuvering characteristics, to improve it. High-lift device could be applied to design of rudder at design stage. Now, we carried out the flow visualization and inversitgation of flow around a flap rudder (trailing-edge flap). Flow visualization results of flap defection shown as the flow around a NACA0020 Flap Rudder will be conducted in a Circulating Water Channel. The purpose of this investigation will be to investigate the development of the separation region on the flap rudder with the variation of angle of attack and determine the angle of attack at which the flow separates and reattaches.

• Advances in aircraft and spacecraft science
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• 제9권2호
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• pp.131-148
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• 2022

The paper presents the surface-modified NACA 2412 airfoil performance with variable cavity characteristics such as size, shape and orientation, by numerically investigated with the pre-validation study. The study attempts to improve the airfoil aerodynamic performance at 30 m/s with a variable angle of attack (AOA) ranging from 0° to 20° under Reynolds number (R_e) 4.4×10⁵. Through passive surface control techniques, a boundary layer control strategy has been enhanced to improve flow performance. An intense background survey has been carried out over the modifier orientation, shape, and numbers to differentiate the sub-critical and post-critical flow regimes. The wall-bounded flows along with its governing equations are investigated using Reynolds Average Navier Strokes (RANS) solver coupled with one-equational transport Spalart Allmaras model. It was observed that the aerodynamic efficiency of cavity airfoil had been improved by enhancing maximum lift to drag ratio ((l/d) max) with delayed flow separation by keeping the flow attached beyond 0.25C even at a higher angle of attack. Detailed investigation on the cavity distribution pattern reveals that cavity depth and width are essential in degrading the early flow separation characteristics. In this study, overall general performance comparison, all the cavity airfoil models have delayed stalling compared to the original airfoil.

• 한국정보과학회논문지:컴퓨팅의 실제 및 레터
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• 제14권9호
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• pp.901-905
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• 2008

본 논문에서는 무선 센서 네트워크 환성에서 싱크홀 공격을 탐지할 수 있는 방안을 제시한다. 싱크홀 공격은 네트워크를 흐르는 패킷들이 공격자를 통과하도록 하는 공격이다. 따라서 이는 다양한 공격으로 확장될 수 있다. 본 논문에서는 링크 품질 지표에 기반한 라우팅을 수행하는 네트워크에서 싱크홀 공격 방법들을 분석하고 각 공격방법에 따라 공격을 탐지하기 위한 방안들을 제시한다. 제안하는 싱크홀 공격 탐지 방법은 링크 품질 지표에 기반한 동적 라우팅 프로토콜을 사용하는 모든 센서 네트워크에 적용할 수 있으며 소수의 공격 탐지 노드를 사용하여 싱크홀 공격의 탐지가 가능함을 알 수 있다.

• 수산해양기술연구
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• 제26권4호
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• pp.333-340
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• 1990

평판형과 만곡형전개판 주위에서의 유체특성을 파악하기 위하여 회유수조에서 수조기포법에 의한 하시화실험을 유속 0.05 및 0.1m/sec, 영각과 타임라인에 대해서 실시하였다. 그 결과를 요약하면 다음과 같다. 1. 만곡형전개판에서의 유선은 영각 20。까지는 균일한 분포를 이루다가 영각 25。에서 후면에 인접한 유선이 익현장의 1/2지점에서부터 작은 과가 발생되기 시작하고, 영각 30。에서는 익현자의 1.3지접에서 박리가 시작되며 인접한 유선은 전개판의 후면쪽으로 휘어들어가고, 그리고 영각 35。이상에서는 전연에서부터 박리가 시작되며 영각이 증가할수록 박리층이 증가하는 것으로 나타났다. 2. 평판형전개판에서는 영각 20。부터 전연에서 과와 박리가 발생하며, 박리층은 만곡형과 마찬가지로 영각에 비례하는 것으로 나타났다. 3. 후연에서 발생한 과의 크기가 전연의 것보다 약 2~3배 큰 것으로 나타났다. 4. 전개판의 후연에서 유선은 양 전개판 모두 전개판의 방향과 같은 방향으로 흐르다가 점차 유체흐름과 같은 방향이 되는 것으로 나타났다. 5. 전개판 전후면에서의 유속차는 영각 0。~30。에서 점차 증가하다가 영각 35。이상에서는 그 차가 비슷하게 나타났다. 6. 영각 20~30。에서 전후면의 유속차는 만곡형의 경우 후면의 유속이 전면보다 약 1.4~1.5배 빠르게 나타났으며, 평판형은 약 1.2배 빠르게 나타났다.