• 대한기계학회논문집A
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• 제26권11호
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• pp.2442-2449
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• 2002

This paper provides an reference stress based J estimation equation fur cylinders with finite internal axial surface cracks under internal pressure. In part 1, the J estimation equation based on deformation plasticity using Ramberg-Osgood (R-0) materials is proposed. In this paper, the developed CE/EPRI -type solutions ale then re-formulated based on the reference stress concept. Such a re-formulation provides a simpler equation for J. estimation are then further extended to combined internal pressure and bending. The proposed reference stress based J estimation equation is compared with elastic-plastic 3-D FE results using actual stress-strain data for a Type 304 stainless steel. Good agreement between the FE results and the proposed reference stress based J estimations provides confidence in the use of the proposed method to elastic -plastic fracture mechanics of pressurised piping.

• 한국기계가공학회지
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• 제3권1호
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• pp.72-78
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• 2004

In this paper, mechanical behaviors of developed pedicle screw system, made of bio-mechanical materials(Ti-6Al-4V, Grade 5), ale predicted using FEM analysis. As a first step, morphologic construction of normal Korean spines and surgical operation convenience are considered to design optimum pedicle screw system. In this step, various design variables are considered as design parameters to develop optimized models. As a next step, tension and bending tests are performed to improve the structural performance of the developed system using finite element method. In this step, required Static compression and bending test specifications by ASTM F-04 25 04 01 are applied to understand the bio-mechanical behaviors of the designed spinal implant system under various load types. As the results of this research, it is possible to develop efficient pedicle screw system, having enough rigidity and fixation to stand any spinal damage under allowable stress conditions.

• 한국군사과학기술학회지
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• 제20권3호
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• pp.384-392
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• 2017

A linear explosively formed penetrator(LEFP) is a modification of the explosively formed penetrator(EFP). An EFP is axisymmetric and has a dish-shaped liner while LEFP has a rectangular-shaped liner with curved cross section. Upon detonating LEFP forms laterally wide projectile like blade, leaving a long penetration hole on the target. On the other hand, a long-rod tungsten heavy alloy(WHA) penetrator is one of the major threats against most of the ground armored vehicles. In this paper, the feasibility of using an LEFP in protecting against a long-rod WHA penetrator by colliding LEFP into the threat was investigated through a set of numerical simulations. In this study, a scale-down WHA penetrator with length to diameter ratio(L/D) of 10.7 and 7.0 mm diameter was used to represent a long-rod WHA penetrator. LS-DYNA and Multi-Material ALE technique were employed for the simulation. For estimation of the protection effect by LEFP, residual penetration depths into RHA by the threat were compared according to various impact locations against the threat.

• 대한기계학회논문집A
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• 제34권1호
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• pp.117-124
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• 2010

현재까지 소형항공기의 조류충돌 문제는 상대적으로 낮은 비행속력과 개인용 목적의 운용 탓에 항공기 개발 및 운용 시의 중요 문제로 다루어지지 않았다. 따라서 일반적으로 FAR 23의 커뮤터급이나 FAR 25급 중, 대형 항공기와 달리 조류충돌에 대한 안전성 입증 규정이 적용되지 않았던 게 사실이다. 그러나 지점 간 운송수단인 에어택시(Air-taxi)로의 활용과 충격에 상대적으로 취약한 복합재료의 구조재료로의 적용이 확대된 VLJ(Very Light Jet)의 급격한 수요 증가에 대한 예측은 FAR 23 일반 및 실용기급 항공기의 조류충돌에 대한 안전성 향상에 대한 필요성을 증대시키는 원인으로 작용할 것이다. 본 연구는 복합재로 제작된 주익의 조류충돌 안전성 및 구조효율성을 평가하기 위해 복합재와 금속재가 적용된 소형항공기의 주익 앞전의 조류 충돌시의 안전성에 대한 외연적 유한요소 해석 결과를 비교하는 과정을 담고 있다.