• Advances in aircraft and spacecraft science
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• 제5권3호
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• pp.349-362
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• 2018

A non-linear numerical simulation technique for predicting the unsteady performances of an airbreathing engine is developed. The study focuses on the simulation of integrated propulsion systems, where a closer coupling is needed between the airframe and the engine dynamics. In fact, the solution of the fully unsteady flow governing equations, rather than a lumped volume gas dynamics discretization, is essential for modeling the coupling between aero-servoelastic modes and engine dynamics in highly integrated propulsion systems. This consideration holds for any propulsion system when a full separation between the fluid dynamic time-scale and engine transient cannot be appreciated, as in the case of flow instabilities (e.g., rotating stall, surge, inlet unstart), or in case of sudden external perturbations (e.g., gas ingestion). Simulations of the coupling between external and internal flow are performed. The flow around the nacelle and inside the engine ducts (i.e., air intakes, nozzles) is solved by CFD computations, whereas the flow evolution through compressor and turbine bladings is simulated by actuator disks. Shaft work balance and rotor dynamics are deduced from the estimated torque on each turbine/compressor blade row.

• 대한토목학회논문집
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• 제14권4호
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• pp.839-846
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• 1994

본 논문에서 수지형 하천내 1차원 부정류 흐름해석을 위한 알고리즘을 개발하였다. 이 해석 알고리즘은 수지형 하천내 부정류의 흐름을 각각의 지류내 단면간에는 연속방정식과 모우멘트 방정식을 적용하고 합류점과 분류점에서는 연속방정식과 에너지방정식을 적용하여 유한차분화한후, 이에 적합한 순환방정식을 도출하여 적용하였으며, 이때 순환계수들은 합류하는 하천단면, 분류하는 하천단변, 합류점, 분류정에 따라 각각 다르게 결정토록 하였다. 이와같은 순환계수 및 순환방정식을 이용하여 수지형 하천내 흐름해석을 단일 하천내 흐름해석과 동일하게 전진법에서는 순환계수를 계산하고, 후진법에서는 순환방정식의 해를 구하는 것이 가능하도록 하였다. 이에 따라 흐름해석을 위한 컴퓨터 저장용량도 $2N{\times}2N$ 행렬로부터 $2N{\times}4$ 행렬로 줄이도록 하였고 계산시간도 상당히 절약하였으며 이때 N은 수지형 하천내 흐름특성인 유량 및 수위를 결정해야하는 절점을 나타낸다. 이와같이 제안된 알고리즘을 이용하여 수지형 하천내 부정류 흐름을 개인용 컴퓨터등을 이용하여 효율적이며 정확하게 해석할 수 있다.

• Ecology and Resilient Infrastructure
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• 제10권4호
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• pp.217-225
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• 2023

본 연구에서는 금강 장동지구를 대상으로 홍수완충공간을 오프라인 저류지로 조성하여 운영하는 경우에 대해 홍수위 저감 효과를 1차원 부정류 수치모의를 통해 분석하였다. 특히 오프라인 저류지의 횡월류 위어 높이와 폭 (길이)의 변화에 따른 수위변화의 민감도를 분석하여 홍수관리시설 (제방) 설계에 필요한 정보를 정량적으로 제공하였다. 첨두 홍수량 및 홍수위를 기준으로 오프라인 저류지의 홍수조절효과를 분석한 결과, 공간적으로는 홍수완충공간 조성 예정지와 하류구간에서 홍수조절효과가 확인되었으며, 특히 하류에서 가장 큰 홍수저감 효과가 나타나는 것을 확인할 수 있었다. 횡월류 위어의 설계 조건별로는 50년 빈도 홍수위 기준의 월류고와 125 m의 횡월류 위어 폭 (길이)을 고려한 조건에서 가장 큰 홍수저감 효과가 나타났다. 오프라인 저류지 조성으로 최대홍수량 도달 시간이 지연되는 효과 또한 부정류 모의를 통해 제시하였다.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2006년도 추계 학술대회논문집
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• pp.18-21
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• 2006

This paper investigates LES of turbulent combustion flow based on 2-scalar flamelet approach, where a G-equation and a conserved scalar equation simulate a propagation of premixed flame and a diffusion combustion process, respectively. The turbulent SGS modeling on these flamelet combustion approach is also researched. These LES models are applied to an industrial flows in a full scale gasturbine combustor with premixed and non-premixed flames. The numerical results predict the characteristics of experiment temperature profiles. Unsteady features of complex flames in combustor are also visualized.

• Wind and Structures
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• 제38권2호
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• pp.147-160
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• 2024

The aerodynamic force is a significant component that influences the stability and safety of structures. It has unstable properties and depends on computer precision, making its long-term prediction challenging. Accurately estimating the aerodynamic traits of structures is critical for structural design and vibration control. This paper establishes an unsteady aerodynamic time series prediction model using Long Short-Term Memory (LSTM) network. The unsteady aerodynamic force under varied Reynolds number and angles of attack is predicted by the LSTM model. The input of the model is the aerodynamic coefficients of the 1 to n sample points and output is the aerodynamic coefficients of the n+1 sample point. The model is predicted by interpolation and extrapolation utilizing Unsteady Reynolds-average Navier-Stokes (URANS) simulation data of flow around a circular cylinder, square cylinder and airfoil. The results illustrate that the trajectories of the LSTM prediction results and URANS outcomes are largely consistent with time. The mean relative error between the forecast results and the original results is less than 6%. Therefore, our technique has a prospective application in unsteady aerodynamic force prediction of structures and can give technical assistance for engineering applications.

• 한국수자원학회:학술대회논문집
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• 한국수자원학회 2005년도 학술발표회(1)
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• pp.138-140
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• 2005

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.848-854
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• 2006

In this study, a computational analysis system has been developed in order to investigate flow-induced vibration(FIV) phenomenon for general stator-rotor cascade configurations. Relative movement of the rotor with respect to stator is reflected by modeling independent two computational domains. Fluid domains are modeled using the unstructured grid system with dynamic moving and local deforming methods. Unsteady, Reynolds-averaged Navier-Stokes equations with one equation Spalart-Allmaras and two-equation SST $k-\omega$ turbulence models are solved for unsteady flow problems. A fully implicit time marching scheme based on the Newmark direct integration method is used flow computing the coupled governing equations of the fluid-structure interaction problem. Detailed FIV responses for different flow conditions are presented with respect to time and vibration characteristics are also physically investigated in the time domain.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 춘계학술대회논문집B
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• pp.247-252
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• 2001

In this paper, dynamic modeling and its analysis for the PIG flow through $90^{\circ}$ curved pipe with compressible and unsteady flow are studied. The PIG dynamics model is derived by using Lagrange equation under assumption that it passes through 3 different sections in the curved pipeline such that it moves into, inside and out of the curved section. The downstream and up stream flow dynamics including the curved sections are solved using MOC. The effectiveness of the derived mathematical models is estimated by simulation results for a low pressure natural gas pipeline including downward and upward curved sections. The simulation results show that the proposed model and solution can be used for estimating the PIG dynamics when we pig the pipeline including curved section.

• 한국전산유체공학회지
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• 제10권4호통권31호
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• pp.24-31
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• 2005

A dynamic simulation on the missile staging system is conducted with numerical techniques. Both Euler equations and Navier-Stokes equations are numerically solved respectively. The dynamic simulation of two moving bodies is fully integrated into the computational fluid dynamics solution procedure. The Chimera grid scheme is applied in this simulation for unsteady supersonic flow analysis with dynamic modeling. The objective of the study is to investigate the problem pertaining to possible unstability in missile staging. In addition, the computational comparison between in viscid and viscid flow solvers is also performed in this study.

• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2011년도 춘계학술대회 초록집
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• pp.87.2-87.2
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• 2011

1kW급 가정용 연료전지 블로어는 다이어프램방식에 의해 고압 및 일정유량의 가스를 이송시키는 역할을 하고 있다. 본 연구에서는 연료전지 중 연료승압블로어를 대상으로 흡입 및 토출시의 다이어프램 캐비티(Cavity) 내의 공기유동 특성을 수치해석을 적용하여 평가하였다.