• The KIPS Transactions:PartA
• /
• v.9A no.4
• /
• pp.405-412
• /
• 2002

The embedded system has less fast CPU and lower memory than PC(personal Computer) or Workstation system. Therefore embedded operating is system is designed to efficiently use the limited resource in the system. Virtual memory management or the embedded linux have a low efficiency when page fault is occurred to get a data from I/O device. Because a data is moving from the swap device to main memory. This paper suggests virtual memory compression algorithm for improving in virtual memory management and capacity of space. In this paper, we present a way to performance implement a virtual memory compression system that achieves significant improvement for the embedded system.

• Proceedings of the Korean Information Science Society Conference
• /
• 2010.06b
• /
• pp.363-367
• /
• 2010

임베디드 시스템 가상화는 PDA, 스마트 폰과 같은 장비에서 다양한 운영체제 및 응용프로그램이 동작하도록 컴퓨팅 자원에 대한 추상화를 제공한다. 반면 한정된 자원을 여러 가상 머신이 분할하여 사용함으로써 자원량의 제한이 더욱 심화된다. 특히, 메모리의 부족은 프로세스 실행에 반드시 필요한 자원으로 반드시 해결되어야 하는 문제이다. 본 논문은 메모리의 부족을 해결하기 위해 불필요한 메모리 공간에 대한 압축을 제안한다. 이는 가상화로 인한 메모리 분할과 프로세스의 메모리 상주 등의 이유로 인한임베디드 시스템 가상화 환경에서의 메모리 부족을 해결할 수 있다. 본 논문은 이 메모리 압축 기법을 기술하고, 실제 가상화된 임베디드 시스템에서 경험한 메모리 부족 문제를 보인다. 이를 통해 메모리 절약 기법의 당위성을 증명하고, 향후 가상 머신 모니터에서의 메모리 압축 기법의 구현과 성능 평가의 기초를 다진다.

• Journal of the Korean Society of Propulsion Engineers
• /
• v.21 no.5
• /
• pp.71-79
• /
• 2017

A numerical analysis of the liquid-gas two-phase flows has been conducted. The incompressible equations of the two-phase flows were solved by the artificial compressibility method with the CLSVOF interface capturing method. To analyze the grid dependency of CLSVOF, a numerical analysis of Zalesak's disk and three-dimensional liquid deformation problem were carried out, and the reconstruction of deformation was investigated. The Rayleigh-Taylor instability was numerically analyzed by applying the equations of incompressible two-phase flow, and the surface instability was observed.

• Journal of the Korean Society for Aeronautical & Space Sciences
• /
• v.49 no.6
• /
• pp.449-456
• /
• 2021

In this paper, we present a strategy to extend solution capability of an existing low Mach number preconditioned compressible solver to incompressible flows with a little modification. To this end, the energy equation that is of the same form of the total energy equation of compressible flows is used. The energy equation is obtained by a linear combination of the thermal energy equation, the continuity equation and the mechanical energy equation. Subsequently, a modified artificial compressibility method in conjunction with a time marching technique is applied to these incompressible governing equations for steady flow solutions. It is found that the Roe average of the common governing equations is equally valid for both the compressible and incompressible flow conditions. The extension of an existing compressible solver to incompressible flows does not affect the original compressible flow analysis. Validity for incompressible flow analysis of the extended solver is examined for various inviscid, laminar and turbulent flows.

• 한국전산유체공학회:학술대회논문집
• /
• 2008.03b
• /
• pp.614-617
• /
• 2008

An unstructured hybrid mesh flow solver has been developed for the simulations of three dimensional steady and unsteady incompressible flow fields. The incompressible Navier-Stokes equations with an artificial compressibility method were discretized by using a node-based finite-volume method. For the unsteady time-accurate computation, a dual-time stepping method was adopted to satisfy a divergence free flow field at each physical time step. The one equation Spalart-Allmaras turbulence model has been adopted to solve the high-Reynolds number flow fields. This method has been applied to calculate the steady flow fields around submarine configurations and unsteady flow fields around a 3-D infinite cylinder.

• 한국전산유체공학회:학술대회논문집
• /
• 2010.05a
• /
• pp.389-396
• /
• 2010

In this paper, a new computational code was developed using Chorin's artificial compressibility method to solve the two-dimensional incompressible Navier-Stokes equations. In spatial derivatives, Roe's flux difference splitting was used for the inviscid flux, while central differencing was used for the viscous flux. Furthermore, AF-ADI with dual time stepping method was implemented for accurate unsteady computations. Two-equation turbulence models, Menter's $k-{\omega}$ SST model and Coakley's $q-{\omega}$ model, hae been adopted to solve high-Reynolds number flows. A number of numerical simulations were carried out for steady laminar and turbulent flow problems as well as unsteady flow problem. The code was verified and validated by comparing the results with other computational results and experimental results. The results of numerical simulations showed that the present developed code with the artificial compressibility method can be applied to slve steady and unsteady incompressible flows.

• Journal of computational fluids engineering
• /
• v.13 no.3
• /
• pp.35-43
• /
• 2008

A methodology for the simulation of compressible high Reynolds number flow over rigid and moving bodies on a structured Cartesian grid is described in this paper. The approach is based on a modified version of the Brinkman Penalization method. To avoid oscillations in the vicinity of the body and to simulate shcok-containing flows, a Weighted Essentially Non-Oscillatory scheme is used to discretize the spatial flux derivatives. For high Reynolds number viscous flow, two turbulence models of the two-equation Menter's SST URANS model and a two-equation Detached Eddy Simulation are implemented. Some simple flow examples are given to assess the accuracy of the technique. Finally, a moving grid capability is demonstrated.

• 한국전산유체공학회:학술대회논문집
• /
• 2007.10a
• /
• pp.200-208
• /
• 2007

A methodology for the simulation of compressible high Reynolds number flow over rigid and moving bodies on a structured Cartesian grid is described in this paper. The approach is based on a modified version of the Brinkman Penalization method. To avoid oscillations in the vicinity of the body and to simulate shcok-containing flows, a Weighted Essentially Non-Oscillatory scheme is used to discretize the spatial flux derivatives. For high Reynolds number viscous flow, two turbulence models of the two-equation Menter's SST URANS model and a two-equation Detached Eddy Simulation are implemented. Some simple flow examples are given to assess the accuracy of the technique. Finally, a moving grid capability is demonstrated.

• Proceedings of the Korea Information Processing Society Conference
• /
• 2005.11a
• /
• pp.1483-1486
• /
• 2005

일반적으로 응용 프로그램의 메모리 요구를 배치 전에 평가하는 것은 많은 어려움이 따르기 때문에 주기억장치의 부족을 초래한다. 또한 임베디드 시스템의 디스크와 가상 메모리의 결핍은 out-of-memory 에러가 발생할 때 응용이 확장되기 위한 swap 공간이 없어 시스템이 붕괴되고 가상 기억장소로부터의 보호가 없어 세그먼트가 그 바운드를 초과했다는 것조차 발견되지 않으므로 붕괴 전의 교정 동작이 불가능하게 한다. 시스템 붕괴가 치명적인 손실이 될 수 있는 임베디드 시스템에서 Out-of-memory 에러는 비신뢰성을 보이는 중요한 원인이 된다. 본 논문에서는 컴파일러에 의한 런타임 조사 코드를 사용함으로써 out-of-memory 에러들이 발생하기 바로 전에 발견하는 런타임 조사와 out-of-memory 이후 죽은 변수 같은 사용되지 않는 공간과 살아있는 변수의 압축으로 자유롭게 된 공간으로 스택이나 힙 세그먼트를 확장시키는 공간 재활용과 데이터 압축 기법으로 시스템 신뢰성을 개선하는 방법을 연구하였다.

• KSCE Journal of Civil and Environmental Engineering Research
• /
• v.13 no.4
• /
• pp.87-99
• /
• 1993

The computer program, MFPD, which is used to backcalculate the layer moduli of asphalt concrete pavement system is modified by contemplating the depth to virtual bedrock in this study. An algorithm to estimate the depth to virtual bedrock is developed through the analysis of FWD impulse load duration and the compression wave velocity of ground. For verification of the modified MFPD, FWD is fabricated and then FWD field tests and verification tests are carried out at the test sites. Plate loading tests and surface wave propagation tests are performed at FWD test sites. Laboratory tests (Marshall stability tests, unconfined compression tests) for sampled asphalt concrete specimens are also carried out. From comparison analysis, the validity and applicability of the modified MFPD are verified.