• 제목/요약/키워드: Projectile

검색결과 399건 처리시간 0.025초

표면처리된 Al 5083-H131 합금의 고속 충격 거동에 관한 연구 (A Study on the fracture behavior of surface treated Al 5083-H131 alloy under the high velocity impact)

  • 손세원;김희재;홍성희;황도연
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1997년도 추계학술대회 논문집
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    • pp.820-824
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    • 1997
  • In order to investigate the effect of surface treatment(Anodizing) and rolling in Al 5083-H131 alloy, ballistic testing was conducted. Ballistic resistance of these materials. was measured by protection ballistic limit(V$_{50}$), a statical velocity with 50% probability for incomplete penetration. Fracture behaviors and ballistic tolerance, described by penetration modes, are observed respectfully, resulting from V$_{50}$ test and Projectile Through Plates(PTP) test at velocities greater than V$_{50}$. PTP tests were conducted with 0$^{\circ}$obliquity at room temperature were also conducted with projectiles that were able to achieve near or complete penetration during PTP tests. Resistance to penetration, and penetration modes of Al 5052-H34 alloy, compared to those of Al 5083-H131 alloy.alloy.

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Design of an Alpine Skiing Game Using ActionScript 3.0

  • Bai-Tiantain, Bai-Tiantain;Park, Jong-Hoon;Kim, Chul-Won
    • Journal of information and communication convergence engineering
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    • 제10권2호
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    • pp.168-174
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    • 2012
  • Flash is the most popular 2D animation and game development software, supporting vector and media technology at the core, which enables the development of small and pithy games. It is widely used in Web animation, courseware, TV commercials, game development, and other works of design. In this paper, we propose a control movement function and auxiliary functions for an alpine skiing game based on ActionScript 3.0. The control movement function is designed with moving phases (i.e., free fall, sliding, projectile, and landing). The auxiliary functions include drawing path, start/restart movement, and saving the highest score. In addition, for the visual design of our game, we designed animations in connection with a character and background. In order to facilitate testing the friction, users can input a chosen friction value. Without user input, the friction default is set at 0.97.

차량용 2축구동장치를 위한 BLDC 서보제어시스템 설계 (The Design BLDC Servo Control System for 2-Axis Actuator Mounted on Vehicle)

  • 주재훈;심동석;이규환;최중경
    • 한국정보통신학회:학술대회논문집
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    • 한국해양정보통신학회 2011년도 춘계학술대회
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    • pp.191-194
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    • 2011
  • 이 논문은 BLDC 서보모터를 사용하여 고각 방위각 2축 무기발사체 시스템을 구동하기 위한 TMS320F28335 DSP 제어기와 MOSFET 인버터 드라이버 설계에 관한 논문이다.

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압축가스 유량 제어밸브의 유동특성 연구 (A study on the flow characteristics of compressed-gas flow rate control valve)

  • 김준범;박원규;한명철;정찬희;안재열
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 추계 학술대회논문집
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    • pp.25-28
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    • 2004
  • The purpose of this paper is to present essential numerical data of FCV(Flow rate Control Valve) which is used in a projectile ejection system for a underwater vehicle. A commercial CFD code is applied to analyze the 3 dimensional viscous compressible flow field within the FCV as four cases of opening rate, 25, 50, 75, and $100\%$. The flow coefficient of each cases are mainly calculated. And other characteristics such as the location of shock wave and total temperature distribution are also determined.

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렘제트탄의 공기역학적 특성 연구 (The Study of Aerodynamic Characteristics for the Ram-jet Projectile)

  • 박순종;신필권;이택상;김경련;박종호;김윤곤
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.751-754
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    • 2002
  • The SFU(Solid Fuel Ram-Jet) propulsion is attractive for projectiles because of the combination of high propulsive performance and low system complexity more than conventional projectiles. The Objective of this research was to characterize the inlet aerodynamic characteristics (centerbody & pilot type) in SFRJ. Diffuser static pressure & combustion chamber pressure was tested and the AoA was changed $0^{\circ}\;and\;4^{\circ}$ at Mach number of 3.0 for performance estimate. The performance study of inlet was carried out with the Schlieren system and Supersonic cold-flow system. A Computational fluid dynamic solution is applied internal flow of inlet and the solutions are compared with experimental results.

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충격파를 동반한 연소현상에 관한 적응 격자 유한요소법 해석 (Adaptive Finite Element Analysis of Shock-induced Combustion)

  • 문수연;이충원;손창현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 추계학술대회논문집B
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    • pp.444-449
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    • 2001
  • A numerical parametric study is conducted to simulate shock-induced combustion with a variation in freestream conditions. A steady combustion front is established if the freestream Mach number is above the Chapman-Jouguet speed of the mixture. On the other, an unsteady reaction front is established if the the freestream Mach number is below or at the Chapman-Jouguet speed of the mixture. The three cases have been simulated for Machs 4.18, 5.11, and 6.46 with a projectile diameter of 15 mm. Machs 4.18 and 5.11 shows an unsteady reaction front, whereas Mach 6.46 represents a steady reaction front. Thus Chapman-Jouguet speed is one of deciding factor for the instabilities to trigger.

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Reactive Ion Scattering of Low Energy Cs+ from Surfaces. A Technique for Surface Molecular Analysis

  • Kang, Heon
    • Bulletin of the Korean Chemical Society
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    • 제32권2호
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    • pp.389-398
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    • 2011
  • Although the currently available surface spectroscopic techniques provide powerful means of studying atoms and simple molecules on surfaces, the identification of complex molecules and functional groups is a major concern in surface analysis. This article describes a recently developed method of surface molecular analysis based on reactive ion scattering (RIS) of low energy (< 100 eV) $Cs^+$ beams. The RIS method can detect surface molecules via a mechanism in which a $Cs^+$ projectile picks up an adsorbate from the surface during the scattering process. The basic principles of the method are reviewed and its applications are discussed by showing several examples from studies of molecules and their reactions on surfaces.

포물선 운동을 이용한 자동차의 떨어진 거리 측정 (Fallen Distance Measure of Vehicle Using Parabolic Motion)

  • 신성윤;표성배;신광성;이현창;이양원
    • 한국컴퓨터정보학회:학술대회논문집
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    • 한국컴퓨터정보학회 2011년도 제43차 동계학술발표논문집 19권1호
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    • pp.63-64
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    • 2011
  • 포물체란 중력이 작용하는 환경에서 어떤 속도로 던져진 물체를 뜻합니다. 예를 들자면, 박찬호 선수가 포수를 향하여 던진 야구공이라든지, 박세리 선수의 스윙으로 그린을 향하여 날아가고 있는 골프공, 그리고 목표물을 향하여 날아가고 있는 포탄은 모두 포물체입니다. 이 물체는 수직방향으로는 중력의 영향을 받고 공기의 저항을 무시한다면 수평방향으로는 힘을 받지 않기 때문에 포물선운동을 한다. 본 논문에서는 포물체의 운동을 이용하여 도로의 일부가 유실되어 없어진 곳을 실험 대상을 한다. 여기에서 속도가 일정하게 달리던 자동차가 유실된 도로의 가장자리를 넘어갔을 때 도로의 가장자리로에서 얼마나 멀리 가서 떨어지는지를 나타내었다.

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Overlapped Electromagnetic Coilgun for Low Speed Projectiles

  • Mohamed, Hany M.;Abdalla, Mahmoud A.;Mitkees, Abdelazez;Sabery, Waheed
    • Journal of Magnetics
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    • 제20권3호
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    • pp.322-329
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    • 2015
  • This paper presents a new overlapped coilgun configuration to launch medium weight projectiles. The proposed configuration consists of a two-stage coilgun with overlapped coil covers with spacing between them. The theoretical operation of a multi-stage coilgun is introduced, and a transient simulation was conducted for projectile motion through the launcher by using a commercial transient finite element software, ANSOFT MAXWELL. The excitation circuit design for each coilgun is reported, and the results indicate that the overlapped configuration increased the exit velocity relative to a non-overlapped configuration. Different configurations in terms of the optimum length and switching time were attempted for the proposed structure, and all of these cases exhibited an increase in the exit velocity. The exit velocity tends to increase by 27.2% relative to that of a non-overlapped coilgun of the same length.

Ballistic behavior of steel sheet subjected to impact and perforation

  • Jankowiak, Tomasz;Rusinek, Alexis;Kpenyigba, K.M.;Pesci, Raphael
    • Steel and Composite Structures
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    • 제16권6호
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    • pp.595-609
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    • 2014
  • The paper is reporting some comparisons between experimental and numerical results in terms of failure mode, failure time and ballistic properties of mild steel sheet. Several projectile shapes have been considered to take into account the stress triaxiality effect on the failure mode during impact, penetration and perforation. The initial and residual velocities as well as the failure time have been measured during the tests to estimate more physical quantities. It has to be noticed that the failure time was defined using a High Speed Camera (HSC). Thanks to it, the impact forces (average and maximum level), were analyzed using numerical simulations together with an analytical description coupled to experimental observations. The key point of the model is the consideration of a shape function to define the pulse loading during perforation.