• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2000년도 춘계학술대회논문집
• /
• pp.1185-1191
• /
• 2000

In general, the strength of hull structures can be estimated from stress evaluation considering static and hydro-dynamic load due to sea-wave. However, war ships such as submarine, have frequently experienced the underwater explosion and local structures of ship as well as hull girder can be damaged by the dynamic response excited from underwater non-contact explosion. When explosion happens at underwater, shock wave is radiated In early short time, then gas bubbles are generated, and expansion and contraction are repeated as they float to the surface. The shock wave causes the damage of equipment and its supporting structures, on the other hand, the hull girder strength can be lost by resonance between bubble pulsation and lowest ship natural vibration period. In this paper, the hydro-Impulse force due to bubble was calculated. Based on these results the hull girder strength of submarine was estimated from transient response analysis by using NASTRAN. Also, shock analysis for some equipment supporting structures was carried out by using DDAM. In order to evaluate the strength of these local structures due to shock wave.

• 한국소음진동공학회논문집
• /
• 제18권2호
• /
• pp.153-159
• /
• 2008

General coil spring has linearity. However, disc spring has non-linearity so that using this non-linearity disc spring can be designed to do shock-absorbing in cases we need because shock response also has non-linearity. By changing the shape and stacking number, it is satisfactory with response of displacement, velocity and acceleration. Conventionally, disc spring was used to control the vibration against huge load and limited space. However, it is limitedly used because of difficulty of the designing guidance. Therefore, disc spring is needed to study further in order to apply it widely. Response of disc spring is compared to response of coil spring by changing $h_o/t$ ratio with computer simulation and the usage of disc spring is increased through analysis of effect of design factors. The purpose of this paper is that the shock response of disc spring is calculated through numerical simulation and effect of $h_o/t$ and stiffness is analyzed to broad usage so that design factor of disc spring is presented.

• 한국해양공학회지
• /
• 제19권1호
• /
• pp.20-25
• /
• 2005

The authors performed the underwater explosion analysis for the liquified oxygen tank - a kind of fuel tank of a mid-size submarine, and tried to verify the structural safety for this structure. First, the authors reviewed the theory and application of underwater explosion analysis, using a Structure-Fluid Interaction technique and its finite element modeling scheme. Next, the authors modeled the explosive and sea water as fluid elements, the LOX tank as structural elements, and the interface between the two regions as the ALE scheme. The effect on shock pressure and impulse of fluid mesh size and shape are also investigated. Upon analysis, it was found that the shock pressure due to explosion propagated into the water region, and hit the structure region. The plastic deformation and the equivalent stress were apparent at the web frame and the shock mount of LOX structure, but these values were acceptable for the design criteria.

• 대한금속재료학회지
• /
• 제50권7호
• /
• pp.539-544
• /
• 2012

Thermal shock behavior of TiN-coated SUS 304 substrate was investigated using a laser ablation method. By short surface ablation with a pulse Nd-YAG laser, considerable surface crack and spalling were observed, whereas there were few oxidation phenomena, such as grain growth of TiN crystallites, nucleation and growth of $TiO_2$ crystallites, which were observed from the coatings quenched from $700^{\circ}C$ in a chamber. The oxygen concentration of the ablated coating surface with the pulse laser also had a lower value than that of the quenched coating surface by Auger electron spectroscopy and electron probe micro analysis. These results were attributed to the fact that the properties of the pulse laser method have a very short heating time and so the diffusion time for oxidation was insufficient. Consequently, it was verified that the laser thermal shock test provides a way to evaluate the influence of the thermal shock load reduced oxidation effect.

• Advances in aircraft and spacecraft science
• /
• 제8권1호
• /
• pp.53-67
• /
• 2021

The increasing interest in the exploration of Mars stimulated the authors to study aerodynamic problems linked to space vehicles. The aim of this paper is to evaluate the aerodynamic effects of a flapped wing in collaborating with parachutes and retro-rockets to reduce velocity and with thrusters to control the spacecraft attitude. 3-D computations on a preliminary configuration of a blunt-cylinder, provided with flapped fins, quantified the beneficial influence of the fins. The present paper is focused on Aerodynamics of a wing section (NACA-0010) provided with a trailing edge flap. The influence of the flap deflection was evaluated by the increments of aerodynamic force and leading edge pitching moment coefficients with respect to the coefficients in clean configuration. The study was carried out by means of two Direct Simulation Monte Carlo (DSMC) codes (DS2V/3V solving 2-D/3-D flow fields, respectively). A DSMC code is indispensable to simulate complex flow fields on a wing generated by Shock Wave-Shock Wave Interaction (SWSWI) due to the flap deflection. The flap angle has to be a compromise between the aerodynamic effectiveness and the increases of aerodynamic load and heat flux on the wing section lower surface.

• 대한기계학회논문집A
• /
• 제40권4호
• /
• pp.415-422
• /
• 2016

충격 가속도가 기계 시스템에 가해지면 시스템의 기능 저하 및 파손이 발생할 수 있다. 이러한 문제점을 방지하기 위하여 감시 정찰 비행기에 장착되는 짐발 구조 시스템은 설계 사양으로 MIL-STD-810G 충격 규격을 반드시 만족해야 한다. 일반적으로 비행기에서 전달되는 충격을 완화하기 위하여 시스템의 기초부에 방진고무가 설치된다. 고무는 비선형 하중-변형 관계를 가지므로 정확한 시스템의 충격 응답 계산이 어렵다. 이를 해결하기 위하여 비선형 특성을 2개의 선형으로 근사화하여 기초부에 충격 가속도를 받는 시스템의 동적 해를 유한요소법으로 구하였다. 그리고 동일한 조건에서 행한 실험과 비교 결과 제안된 해석 방법이 강성과 감쇠에서 비선형성을 갖는 방진고무가 포함된 짐발 구조 시스템의 동적 해석에도 유용함을 입증하였다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2010년도 춘계학술대회 논문집
• /
• pp.584-585
• /
• 2010

• Structural Engineering and Mechanics
• /
• 제74권6호
• /
• pp.737-745
• /
• 2020

Nowadays, composite plates are widely used as high-strength structures to fabricate a dynamic loading-resistant armours. In this study, the shock load is applied by an explosion of spherical TNT charge at a specified distance from the circular composite plate. The composite plate contains a two-layer ceramic-metal armour and a poly-methyl methacrylate (PMMA) target layer. The dynamic behavior of the composite armour has been investigated by measuring the transferred effective stress and maximum deflection into the target layer. For this purpose, the simulation of the blast loading upon the composite structure was performed by using the load-blast enhanced (LBE) procedure in Ls-Dyna software. The effect of main process parameters such as the thickness of layers, and scaled distance has been examined on the specific stiffness of the structure using response surface method. After validating the results by comparing with the experimental results, the optimal values for these parameters along with the regression equations for transferred effective stress and displacement to the target have been obtained. Finally, the optimal values of input parameters have been specified to achieve minimum transferred stress and displacement, simultaneously with reducing the weight of the structure.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2009년도 제33회 추계학술대회논문집
• /
• pp.417-420
• /
• 2009

본 연구의 그라파이트는 로켓 노즐목 재료로 많이 사용되는 것으로써 다른 어떤 내열재료보다 로켓추진기관의 작동시간 동안 그 형상을 유지할 수 있는 삭마저항성과 열전도도가 큰 재료이다. 노즐목으로 사용되는 그라파이트는 내삭마성, 사용가능 온도, 가격, 무게측면에서 유리하지만 열충격 강도가 상대적으로 작기 때문에 설계시 구조적인 안전성을 충분히 확보해야만 한다. 본 연구에서는 로켓 노즐목으로 많이 사용하는 ATJ 그라파이트에 대하여 실험과 해석을 통하여 고온 파괴 인성치를 결정하였으며, 열충격시험 결과를 그라파이트 재료의 비선형성을 고려한 hypo elastic 기법을 이용한 해석적 방법으로 비교하여 해석의 정확성을 확인하였다.

• 한국철도학회논문집
• /
• 제17권2호
• /
• pp.100-105
• /
• 2014

해중철도 부근에서 테러나 사고에 의해 수중폭발이 발생하였을 경우, 함체에 치명적인 손상을 가할 수 있으므로, 충분한 강도를 확보해야 한다. 본 연구에서는 설계 목적으로 해중철도 인근에서 수중폭발이 발생한 경우, 경험에 기초한 공식을 이용하여 충격압을 추정하고, 충격압에 의한 해중철도의 응답을 해석할 수 있는 간이 해석 방법을 제안하였다. 해중철도 함체를 탄성 지지된 보로 이상화하고, 초기 최대 충격압이 작용하는 보에 대해 정적 유한요소해석을 실시한 후, 동하중 계수와 조합함으로 최대 변위 및 굽힘 모멘트를 계산한다. 간이해석 결과는 상용 유한요소해석 소프트웨어를 이용한, 시간에 따른 과도응답해석 결과와 비교하여 양호한 일치를 보임을 확인하였다.