• Title/Summary/Keyword: 충격력 특성

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Biomechanical Evaluation of Trekking Shoes using 3D Bootie Method as Mimics Barefoot Form (맨발 구조를 모사한 3D Bootie 공법을 적용시킨 트레킹화의 생체역학적 특성 평가)

  • Yoo, Chan-Il;Jeon, Keun-Hwan;Won, Yonggwan;Kim, Jung-Ja
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.16 no.7
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    • pp.4689-4696
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    • 2015
  • The purpose of this study was to evaluate biomechanical characteristics of trekking shoes using 3D Bootie method as mimics barefoot form of F Co. that provides the best comfort and plantar pressure dispersion. The control group is normal trekking shoes of M Co. and K Co.. 13 healthy males measured the foot pressure, EMG and GRF. Collected data was analyzed using One-way ANOVA in order to investigate the effects of each trekking shoes. The results are as follows: Trekking shoe of F Co. was significantly wider in contact area than others at MF and significantly lower in maximum force, peak pressure than others at RF. In the case of muscle activity, acted in the same way as the effect of barefoot walking. In the case of GRF, effectively absorbed the impact force, so it is possible to efficient walking. As a result of the analysis, trekking shoe using of 3D Bootie method of F Co. can be efficient walking by reducing the load of foot during walking.

Photodegradation Characterization of Polyolefin Composite (폴리올레핀 복합소재의 UV 광열화 특성)

  • Weon, Jong-Il;Shin, Sei-Moon;Choi, Kil-Yeong
    • Applied Chemistry for Engineering
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    • v.20 no.5
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    • pp.511-516
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    • 2009
  • Photodegradation characteristics of polyolefin composites were studied. Thermogravimetric analysis results suggest that the polyolefin blends used in this study have different amounts of talc. The mechanical behaviors of polyolefin blends, which experienced UV-irradiation in accordance with SAE J1960, are investigated using tensile and Izod impact tests. These results show that as the UV-exposure time increases, a significant drop in the elongation at break and impact strength at a low temperature are observed. This may be explained by the decreases in elastic energy derived from the scission of polymer molecular chains and the low density of entanglement after UV- photodegradation. Scanning electron microscopy observations indicate that no crack and surface damage are observed, while the additional talc particles are exposed, on the UV-exposed surfaces. The exposure of talc particles may be responsible for the discoloration of UV-exposed polyolefin blend surface. Observation using Fourier transform infrared spectroscopy (FT-IR) confirms the presence of photodegradation on the surface of UV-exposed polyolefin blend.

The Study of the Characteristic of Pyrotechnic Separation Devices Using Missile System and Space Craft (우주발사체 및 미사일 시스템에 이용되는 파이로테크닉 분리장치의 특성에 관한 연구)

  • Lee, Yeung-Jo;Kim, Dong-Jin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.208-211
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    • 2007
  • Separation Devices have two functions. These two functions are to bond and to separate two bodies. This paper is about separation devices which use explosives to separate their bodies. Explosive bolt is separated with two bodies when the explosives in the body detonated. The good things of explosive bolt are that it has simple operational system and it is made of few parts. But it has side effects; fragment and pyre-shock. To avoid these side effects gas expansion separation(GES) bolt and pressure cartridge actuation separation(PAS) devices are invented. These use pressure to separate their bodies. The pressure is generated when explosives are burned. But the sizes of PAS devices are bigger than explosive bolts. And GES bolt has a mechanically lower bonding ability than that of explosive bolt. When you design separation devices, it is recommended to know operational system and characteristics of separation devices, to design best one.

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Numerical Investigation of the Lateral Jet Effect on the Aerodynamic Characteristics of the Missile: Part II. Freestream-Jet Angle Effect (측 추력 제트가 미사일의 공력특성에 미치는 영향에 관한 연구 : Part II. 자유류-제트 각 영향)

  • Min, Byung-Young;Lee, Jae-Woo;Byun, Yung-Hwan;Hyun, Jae-Soo;Kim, Sang-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.9
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    • pp.27-34
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    • 2004
  • A computational study on the supersonic flow around the lateral jet controlled missile has been performed. For this purpose a three dimensional Navier-Stokes computer code(AADL3D) has been developed and case studies have been performed by comparing the normal force coefficient and the moment coefficient of a missile body for several parameters such as angles of attack, circumferential jet positions, and spouting jet angles. Missile surface is divided into four regions with respect to the center of gravity, and the normal force and moment distribution at each region are compared. The results show different behavior of the normal force and moment variation according to each parameter. Furthermore, it is shown that the pitching moment can be minimized through proper combination of each parameter.

Nonlinear Aeroelastic Analysis of a Wing with Control Surface Freeplay in Subsonic/Transonic Regions (조종면 유격이 있는 날개의 아음속 및 천음속에서의 비선형 공탄성 해석)

  • Kim, Kyung-Seok;Kim, Jong-Yun;Yoo, Jae-Han;Bae, Jae-Sung;Lee, In
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.4
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    • pp.295-301
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    • 2007
  • The aeroelastic characteristics of a wing with control surface freeplay are investigated. The transonic small disturbance equation is used for unsteady aerodynamic forces in subsonic/transonic region. The fictitious mass method is introduced to apply a modal approach to nonlinear structural models. Nonlinear aeroelastic time responses are calculated by the coupled time integration method. Using these methods, an efficient aeroelastic analysis is achieved for aerodynamic and structural nonlinearities simultaneously. The effects of the aerodynamic nonlinearity, initial flap amplitude, and freeplay magnitude in aeroelastic characteristics are investigated in this study.

Modeling of MR Damper Landing Gear Considering Incompletely Developed Fluid Flow (불완전 발달 유체 유동을 고려한 MR댐퍼 착륙장치 모델링)

  • Lee, Hyo-Sang;Jang, Dae-Sung;Hwang, Jai-Hyuk
    • Journal of Aerospace System Engineering
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    • v.15 no.1
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    • pp.7-18
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    • 2021
  • A semi-active MR damper landing gear is a damper that generates a fluid damping force and a magnetic field control damping force when the MR fluid passes through annular flow paths. In the case of MR fluid passing through annular flow paths, an incompletely developed flow inevitably occurs, causing an error in calculating damper inner forces including the fluid damping force. This error results in an inaccurate design of damper structural parameters and control gain selection, resulting in deterioration of dynamic characteristics and shock absorption performance of the landing gear. In this paper, we derived a mathematical model of an MR damper landing gear considering additional damping force generated in the entrance region of annular flow paths of the MR damper. If the mathematical modeling derived from this paper is applied to the design and optimization process of an MR damper landing gear, excellent performance of the MR damper landing gear is expected.

Dynamic Behavior of External Post-tensioned Non-ballast Steel Plate Girder Railway Bridge (외부 후 긴장된 무도상 철도 판형교 동적 거동)

  • Park, Yong Gul;Park, Young Hoon;Choi, Dong Ho
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.28 no.3A
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    • pp.315-322
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    • 2008
  • The present study applied the external post tensioning reinforcement method for reinforcing a non-ballast steel plate girder railway bridge, and the effects of the strength of tendons and the level of post-tensioning force on the dynamic behavior are experimented and analyzed. According to the results of this study, the natural frequency was increased by the strength of tendons but it was decreased by the rise of post-tensioning force and as a consequence the introduction of post-tensioning force decreased natural frequency slightly. It was analyzed that further study is need to establish the exact relations between post-tensioning force and natural frequency. In addition, it was found that the dynamic displacement, dynamic bending stress and vertical acceleration were decreased by the external post-tensioning. On the other hand, external post-tensioning increased horizontal acceleration by up to 20%, which was around 70% of vertical acceleration. This needs further study.

일체형 샌달용 자동화 MOLD의 게이트 형상 최적화

  • 류미라;이권희;박흥식
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.82-82
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    • 2004
  • 우리나라는 신발 생산 특히 부품소재 부분에서 세계적인 경쟁력을 갖추고 있는 것으로 평가되고 있으며, 이 중 E.V.A midsole은 가볍고 충격흡수성 등과 같은 특성이 매우 우수하여 샌달의 midsole 부품으로 널리 사용되고 있지만 현재의 midsole 제조방식은 생산성의 한계에 직면하고 있다. 즉, 패턴 갑피(upper)와 Phylon mold를 각각 생산한 후 별도의 공정에서 두 제품을 접착하여 샌달을 만들기 때문에 두 제품을 따로 생산하므로 현재와 같은 방식의 제조에 의한 기존 방식의 샌달은 제작비용의 증가 및 생산성 저하 등의 여러 가지 문제점을 가지고 있어 보다 새로운 일체형 자동화 사출 mold에 의한 샌달 제조방식의 필요성이 절실한 실정에 있다.(중략)

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A Study on the Experiments and Characteristics Analysis of the Bellows Type Rodless Cylinder (벨로우즈형 로드리스 실린더 특성해석 및 실험에 관한 연구)

  • Kim, Dong-Soo;Kim, Sung-Jong;Bae, Sang-Kyu
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.973-977
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    • 2004
  • A pneumatic cylinder used to sliding seal which seal the element one to another in relative motion. It is difficult to accuracy control because of adhesion phenomenon. To confirm this phenomenon, it is carried to friction force test and analysis for bellows type rodless cylinder. In the rodless cylinder of this type, friction force test is very important. Through the theoretical analysis of shock absorber obtained the optimal design of bellows type rodless cylinder. As the result of the friction force test, LM Guide type is suitable for work under low friction force.

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Investigation of Transonic and Supersonic Flows over an Open Cavity Mounted on Curved Wall (I) - Steady Flow Characteristics - (곡면상에 설치된 열린 공동을 지나는 천음속/초음속 유동에 관한 연구 (I) - 정상 유동의 특성 -)

  • Ye, A Ran;Das, Rajarshi;Kim, Huey Dong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.39 no.3
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    • pp.231-236
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    • 2015
  • Investigations into cavity flows have been conducted for decades now, most of them being about zero-pressure-gradient flows entering a cavity on a straight wall. However, the flow over curved walls in real-life situations has not been fully investigated. As cavity flows on curved walls exert centrifugal force, these walls are likely to possess different features from straight walls. To verify this possibility, this study investigated cavity flows on curved walls. Using numerical method, the effect of two variables, namely, radius of curvature on a curved wall and inlet Mach number, were investigated for subsonic and supersonic cavity flows. The result demonstrates that the value of the peak pressure generated inside the cavity increases with the decrease in the radius of curvature on a curved wall or an increase in the inlet Mach number. The total pressure loss in the cavity also results in an increase in the cavity drag.