• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.3
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• pp.18-27
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• 2019

The flow mixing characteristics for the heated dual jets were numerically studied by using URANS (unsteady Reynolds-averaged Navier-Stokes). The increased turbulent diffusion was obtained for the compressible flow, and the thermal diffusion of incompressible flow increased more than that of compressible flow. From the results of FFT and phase portraits, periodic and quasi-periodic states were observed as the jet spacing increased. It was observed that linear variations of merging points and combined points were different because unsteady flow determined the flow mixing characteristics for a large jet spacing.

• Proceeding of EDISON Challenge
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• 2012.04a
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• pp.37-40
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• 2012

EDISON CFD 수치 해법 기법을 바탕으로 초음속 유동장 속에서 spike가 부착된 무딘 물체에 대하여, spike 형상 변화에 따른 압축성 효과에 의한 항력 변화 추이를 고찰하였다. Spike의 길이 따른 항력 변화 추이를 살펴보았다. Spike의 길이가 Main body와 특정한 비율을 가질 때 항력이 최소가 된다. 이를 기준으로 spike 길이가 특정 길이만큼 줄어들거나 늘어날 경우에 각각 1.35%, 4.95% 항력이 증가하였다. 이러한 자료들은 초음속 유동장에서 무딘 물체에 가해지는 압축성 효과에 의한 저항을 최소화하기 위한 spike 설계 시 중요한 견해를 제공한다.

• Journal of computational fluids engineering
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• v.19 no.3
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• pp.85-90
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• 2014

The purpose of this study is to develop a new Meshless Method to solve 2-D compressible flow problems numerically. This paper includes a revised Least Square method that improves robustness compared with its original version by removing excessive numerical oscillation which occurs when points are randomly distributed. Numerical analyses of hypersonic flow over a blunt body were carried out using the method, then robustness, accuracy and convergence of their results were compared with those obtained from the original method.

• The Journal of the Acoustical Society of Korea
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• v.43 no.1
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• pp.112-121
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• 2024

The pipping system is widely used in many industries as equipment for transporting fluids over long distances. In high-pressure pipe, as the speed of the fluid increases, a loud noise is generated. Therefore, various studies have been conducted to reduce pipe noise. In this paper, a pipe noise analysis was developed to predict and quantitatively assess the flow-induced vibration and acoustic-induced vibration due to valve flow in high-temperature and high-pressure. To do this, a high-fidelity fluid analysis technique was developed for predicting internal flow in the pipe with valve. In additional, the contribution of compressible/incompressible pressure by frequency band was evaluated using the wavenumber-frequency analysis. To predict a low/middle frequency pipe noise, the vibroacoustic analysis method was developed based on Finite Element Method (FEM). And the pipe noise prediction method for the middle/high frequency was developed based on Statistical Energy Analysis (SEA).

• 한국기계연구소 소보
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• s.19
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• pp.15-21
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• 1989

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.6
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• pp.47-55
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• 2018

In order to determine whether three-dimensional effects exist in a pintle nozzle of axisymmetric shape, a three-dimensional numerical analysis was performed. The compressibility correction was implemented with the k-${\omega}$ SST turbulence model to predict the complex flow separation transition in acceptable accuracy. Recirculation zones were observed at both the front end and rear faces of the pintle, and the flow through the pintle nozzle conveyed complex shock wave structures. Three-dimensional effects that resulted from the reasonable flow separation location were noted, and a trace of the transient pressure increase was observed, mismatched by a two-dimensional axi-symmetric analysis.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.5
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• pp.387-395
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• 2015

A technique for calculating the additive drag of the inlet in supersonic flow was studied using commercial CFD software, STAR-CCM+, which provides a efficient way of 3 dimensional flow analysis with polyhedron-shaped grid system. Three configurations were chosen and applied to the calculation with various flow conditions of two different free stream Mach No. and some mass flow ratios. Comparisons with results from wind tunnel test gave good agreements. Though computation were carried out with the inviscid and compressible flow around the supersonic inlet for the supercritical condition, ignoring the viscous effects is concluded to give little effects on the accuracy of the additive drag calculation and to make the calculation more efficient owing to less effort and time consumed for grid system build-up and for iteration because of less grid number and simpler boundary condition.

• Computational Structural Engineering
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• v.11 no.1
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• pp.90-95
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• 1998

본 고에서는 비압축성 점성유체의 유한요소해석 기법을 소개하였다. 대류항의 상류화 기법으로 안정된 해를 도출할 수 있으며 Penalty 방법에 기반하여 압력항을 지배방정식으로부터 소거함으로써 해석시간과 요구저장공간을 감소시켰다. 실린더 주변의 유동장을 해석하여 와의 방출을 성공적으로 묘사하였으며 항력계수를 17%정도의 오차로 계산하였다. 적응적 요소세분화 기법에 대한 연구를 통해 적절한 오차평가 기법 및 최적의 체눈을 형성하는 기법을 제시하였다. 또한 동적 해석에 적합한 요소재결합 알고리즘에 대한 연구가 진행중이다. 본 고의 결과는 직접적으로 풍공학분야에 사용하기에는 아직 계산 시간의 효율성이나 해의 정확도 및 안정성면에서 무리가 있으나 추가적인 연구를 통하여 해석기법의 개선을 도모하고 컴퓨터 등 계산장비의 급속한 발전으로 장래에 경쟁력을 획득할 수 있을 것으로 기대된다.

• Transactions of the Korean Society of Mechanical Engineers B
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• v.35 no.10
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• pp.1019-1024
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• 2011

The gaseous fuel injection(GFI) type of LPG fuel-supply system is more advantageous than liquefied fuel injection(LFI) from the viewpoint of durability and cost reduction. However, compared with LFI types of LPG fuel-supply systems, in the GFI systems it is difficult to achieve precision fuel metering because of the compressible characteristic of the gaseous fuel. In this study, a Helmholtz resonator is proposed as an appropriate system for precision fuel metering in GFI systems, and the effects of the Helmholtz resonator on the fuel metering are simulated by the commercial flow-network-analysis package Flowmaster.

• Journal of Aerospace System Engineering
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• v.2 no.2
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• pp.20-27
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• 2008

The characteristics of compressible flow are different from those of incompressible flow from the mathematical and physical point of view. Therefore, the way to solve the flowfield is different between compressible flow and incompressible flow. In general, density-based numerical algorithm is mainly used for compressible flow solver development. On the other hand, incompressible flow solver prefers to use pressure-based numerical algorithm. In this research, a compressible Navier-Stokes flow solver is developed by means of extending from pressure-based incompressible numerical algorithm to handle both compressible and incompressible flows using the same flow solver. The present flow solver is tested at various speed ranges and compared with the solutions of density-based compressible flow solver. Numerical results show a good agreement between two flow solvers.