• 한국정보통신학회논문지
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• 제4권4호
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• pp.901-905
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• 2000

본 연구는 미사일 헤드와 같은 돔형의 실린더형 ogive (Cylindrical Ogive)를 타원형 ogive(Elliptical Ogive)로 대치하여 지상의 레이다로부터 미사일의 탐지확률을 줄이는 연구이다. 미사일의 RCS(Radar Cross Section)를 계산하기 위해 GTD(Geometrical Theory of Diffraction)/UTD(Uniform GTD)를 사용하였다. 향후, 형상변경에 따른 미사일 헤드의 공기역학(aerodynamics)적인 타당성 검토가 이루어져야 한다.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2000년도 하계종합학술대회 논문집(1)
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• pp.263-266
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• 2000

An elliptical ogive head for a generic missile is proposed to reduce its detectable probability from a ground defense radar. Numerical RCS results of a generic missile with an elliptical ogive head are evaluated using the GTD/UTD (Geometrical Theory of Diffraction/Uniform GTD). The results are compared with those of a cylindrical ogive head. In the sense of aerodynamics, the Performance evaluation of an elliptical ogive head for a generic missile should be followed.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.3-7
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• 2007

The characteristics of asymmetric vortex and side force of tangent-ogive-cylinder flight vehicle at high angles of attack have been performed by using upwind Navier-Stokes method with the ${\kappa}-{\omega}$ turbulence model. And Asymmetric transition positions are considered for generation of asymmetric vortex.

• 대한기계학회논문집
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• 제18권10호
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• pp.2664-2674
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• 1994

Drag, lift, and pitching moment measurements have been made on a range of slanted-base ogive cylinders, using the KANOMAX wind tunnel and balance system. Test Reynolds numbers(based on model maximum diameter) varied from $0.54{\times}10^{5}{\;}to{\;}1.56{\times}10^{5}$. Crossflow velocity maesurement was conducted by 5-hole pitot tube at $Re_{D}=1.46{\times}10^{5}$. For two base angle $({\theta}=30$ and 45 deg.), aerodynamic forces and moment were measured with increasing angle of attack(0~30 deg.). Two types of wake flow were observed, a quasisymetric turbulent closure or a longitudinal vortex flow. Aerodynamic characteristics differ dramatically between the two wake types. It was found that the drag, lift and pitching moment coefficients increased with increasing angle of attack.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 춘계 학술대회논문집
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• pp.130-133
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• 2007

A two-phase method in CFD has been developed and is applied to model the cavitation flow. The governing equation system is two-phase Navier-Stokes equation, comprised of the mixture mass, momentum and liquid-phase mass equation. It employs an implicite, dual time, preconditioned algorithm using finite difference scheme in curvilineal coordinates and Chien ${\kappa}-{\varepsilon}$ turbulence equation. The experimental cavitating flows around ogive-cylinder and venturi type objects are employed to test the solver. To prove the capabilities of the solver, several three-dimentional examples are presented.

• 한국군사과학기술학회지
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• 제16권5호
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• pp.607-612
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• 2013

The effect of the flow actuator on the asymmetric vortex structure around the ogive-cylinder body with fineness ratio of 4 flying at the speed of Mach 0.1 at angle of attack of 50 degree is studied. The ogive-cylinder model is developed with the actuator placed near the nose tip and numerically simulated using the in-house CFD code named KFLOW. The numerical simulation employs two different actuator modeling: one is the boundary condition given by blowing normal to the surface and another shearing on the surface. The numerical simulation reveals that response of the vortex structure to the actuation is dependent on the type of modeling as well as the strength and direction of the actuation.

• Computers and Concrete
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• 제8권1호
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• pp.111-123
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• 2011

Severe element distortion problem is observed in finite element mesh while performing numerical simulations of high velocity steel projectiles penetration/perforation of concrete targets using finite element method (FEM). This problem of element distortion in Lagrangian formulation of FEM can be resolved by using element erosion methodology. Element erosion approach is applied in the finite element program by defining failure parameters as a condition for element elimination. In this study strain parameters for both compression and tension at failure are used as failure criteria. Since no direct method exists to determine these values, a calibration approach is used to establish suitable failure strain values while performing numerical simulations of ogive-nose steel projectile penetration/perforation into concrete target. A range of erosion parameters is suggested and adopted in concrete penetration/perforation tests to validate the suggested values. Good agreement between the numerical and field data is observed.

• Structural Engineering and Mechanics
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• 제13권6호
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• pp.639-652
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• 2002

The present study aims to improve an existing model for the prediction of deceleration time history, penetration depth and forces on ogive and conical nose shaped missiles under normal impact into geo-material targets. The actual ogive nose shaped missile has been considered in the analysis and the results thus obtained have been compared with the existing model and significant improvements are found. A close proximity in the results has also been observed with the experimental values. The results of ogive nose shaped missile have also been compared with equivalent conical nose shaped missile. Variation of radial stresses along nose length and radial direction has been studied. Effect of CRH on missile penetrating performance has been investigated.

• 한국군사과학기술학회지
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• 제18권5호
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• pp.566-573
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• 2015

The most important factor for the penetration performance of shaped charge is the liner design. By designing the liner to have properties of both high jet tip velocity and long jet break-up time, the better penetration performance could be acquired. Usually it is very difficult to satisfy above two conditions simultaneously. In this study, the liner with the shape of ogive was developed to have relatively larger jet mass compared to the conventional trumpet liner. The designed shaped charge showed jet properties with high jet tip velocity and long jet break-up time by using ogive liner and wave shaper. A commercially available hydro-dynamic code AUTODYN-2D was used for numerical analysis of jet formation. The flash X-ray test and the static penetration test were conducted to verify the results of numerical analysis.

• 한국산학기술학회논문지
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• 제21권6호
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• pp.672-678
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• 2020

국내에서 생산중인 대구경 탄약은 대부분 Ogive 부를 제조하는 방법으로 Press Nosing 공법을 적용하고 있다. Press Nosing 공법은 프레스 공정 전 후 윤활처리 등의 추가적인 공정이 필요한 단점이 있다. 본 연구에서는 이러한 단점을 개선할 수 있는 점진성형 공법 중 하나인 Swaging 공법의 대구경 탄약 적용 가능성을 제시하고자 하였다. 대구경 탄약인 155MM K307 탄체는 Press Nosing 공정을 적용하는 대표적인 제품으로, 본 연구에서는 K307 탄체의 Sub-scale 시험품을 제작하여 Swaging 공정을 적용한 소성가공 실험을 실시하였다. 최종 성형 치수를 만족하는 단면감소율 75 % 까지 소성가공이 가능한지 여부 및 Swaging 성형으로 제작된 제품의 치수만족 여부, 제품 결함 발생 여부, 단면감소율에 따른 경도 변화, 두께의 증가 등을 고찰하였다. 시험을 통해 단면적 감소율에 따라 비례적으로 경도가 증가하여 단면적 감소율 75 %에서 경도는 HV 335 이상 증가하는 것을 확인하였다. 소재두께 변화량은 이론적 계산값과 유사한 경향을 보였으며 단면 감소율 75 %에서 두께 증가율은 65.4 %로 비례함을 확인하였다.