• Title/Summary/Keyword: FORTRAN interface

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Implementation and Performance Analysis of High Performance Computing Library for Parallel Processing (병렬처리를 위한 고성능 라이브러리의 구현과 성능 평가)

  • 김영태;이용권
    • Journal of KIISE:Computer Systems and Theory
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    • v.31 no.7
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    • pp.379-386
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    • 2004
  • We designed a portable parallel library HPCL(High Performance Computing Library) with following objectives: (1) to provide a close relationship between the parallel code and the original sequential code that will help future versions of the sequential code and (2) to enhance performance of the parallel code. The library is an interface written in C and Fortran programming languages between MPI(Message Passing Interface) and parallel programs in Fortran. Performance results were determined on clusters of PC's and IBM SP4.

C-FORTRAN 혼합언어(Mixed Language) 프로그래밍

  • 최창근
    • Computational Structural Engineering
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    • v.2 no.3
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    • pp.26-29
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    • 1989
  • 두가지 또는 그 이상의 언어를 각각의 언어의 장점만을 취하여 혼합한다면 매우 효율적인 프로그램을 만들 수 있게 된다. 이 글에서는 공학문제 해결에 많이 쓰여온 FORTRAN과 C언어의 PC에서의 Interface에 대해 논하고 구조공학 분야에서의 활용방안의 일단을 제시하고자 한다.

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Data-Exchange Interface Design of Pre-& Post-Processing System for Finite Element Structural Analysis Program (유한요소 구조해석 프로그램의 전후처리 접속장치의 설계)

  • Shin, Young-Shik;Suh, Jin-Kook
    • Journal of the Korean Society of Industry Convergence
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    • v.2 no.2
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    • pp.41-49
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    • 1999
  • In general, FORTRAN is used for numerical analysis and OPS5 or LISP is used for expert systems, This causes problems at the interface because the various applications require different computing languages or environments. This paper describes the approach used to take AutoCAD as a user-interface for an existing finite element structural analysis package. Some principles concerning database management related to data-exchange interface of pre- and post-processing system for FORTRAN structural analysis program are discussed, and numerical examples demonstrate the power of the combination of these programs.

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Articulated Rotor/Aerodynamics Co-Simulation Using FMI Standard (FMI 표준을 활용한 관절형 로터/공력 연계시뮬레이션)

  • Paek, Seung-Kil;Park, Joongyong
    • Journal of Aerospace System Engineering
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    • v.9 no.4
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    • pp.1-7
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    • 2015
  • The purpose of this research is to develop co-simulation methodology of codes developed in different modeling and simulation environment. We develop aerodynamic FMU(Functional Mock-up Unit) meeting FMI(Functional Mock-up Interface) specification version2 utilizing Legacy FORTRAN aerodynamic code based on unsteady vortex lattice method. It is concluded that making FMU is possible utilizing Legacy code made in any language which can be compiled and linked with object in FMI API coded in C language. This paper explains QTronic's method of using FMU SDK(Software Development Kit) and suggestion for using FORTRAN properly. Finally, we make articulated rotor/aerodynamics co-simulation by integrating aerodynamics FMU and rotor FMU developed by Modelica.

An Electric Arc Furnaces Load Model for Transient Analysis (과도현상 해석을 위한 EAFs 부하 무델의 개발)

  • Jang, Gilsoo;Venkata, S.S.;Kwon, Sea-Hyuk
    • The Transactions of the Korean Institute of Electrical Engineers A
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    • v.48 no.3
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    • pp.197-202
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    • 1999
  • Electric arc furnaces (EAFs) use bulk electrical energy to create heat in metal refining industries. The electric arc process is a main cause of the degradation of the electric power quality such as voltage flicker due to the interaction of the high demand currents of the load with the supply system impedance. The stochastic models have described the aperiodic physical phenomena of EAFs. An alternative approach is to include deterministic chaos in the characterization of the arc currents. In this parer, a chaotic approach to such modeling is described and justified. At the same time, a DLL(Dynamic Link Library) module, which is a FORTRAN interface with TACS (Transient Analysis of Control Systems), is developed to implement the chaotic load model in the Electromagnetic Transients Program (EMTP). The details of the module and the results of tests performed on the module to verify the model and to illustrate its capabilities are presented in this paper.

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Performance Simulation of A Turbojet Engine Using $SIMULINK^{\circledR}$ ($SIMULINK^{\circledR}$를 이용한 터보제트 엔진의 성능모사)

  • 공창덕;박종하;기자영;강명철
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.05a
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    • pp.110-114
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    • 2003
  • In this study, a performance simulation program for a turbojet engine using SIMULINK, which can provide the GUI(Graphic User Interface) environment, was newly proposed. Performance analysis results using the SIMULINK performance program were compared with them using the FORTRAN performance program that was previously developed. According to comparison result, it was noted that performance analysis results between two programs have little bit big difference. This difference seems to be due to different component matching algorithm at each program, it will be improved later.

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Development of a flux emergence simulation using parallel computing

  • Lee, Hwanhee;Magara, Tetsuya
    • The Bulletin of The Korean Astronomical Society
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    • v.44 no.2
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    • pp.71.1-71.1
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    • 2019
  • The solar magnetic field comes from the solar interior and is related to various phenomena on the Sun. To understand this process, many studies have been conducted to produce its evolution using a single flux rope. In this study, we are interested in the emergence of two flux ropes and their evolution, which takes longer than the emergence of a single flux rope. To construct it, we develop a flux emergence simulation by applying a parallel computing to reduce a computation time in a wider domain. The original simulation code had been written in Fortran 77. We modify it to a version of Fortran 90 with Message Passing Interface (MPI). The results of the original and new simulation are compared on the NEC SX-Aurora TSUBASA which is a vector engine processor. The parallelized version is faster than running on a single core and it shows a possibility to handle large amounts of calculation. Based on this model, we can construct a complex flux emergence system, such as an evolution of two magnetic flux ropes.

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Development of a process control package using PC (PC를 이용한 자동제어시스템 개발)

  • 구영재;이준서;이인범;장근수
    • 제어로봇시스템학회:학술대회논문집
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    • 1991.10a
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    • pp.322-326
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    • 1991
  • A real time process control package was developed in an INTEL 80386 based PC and MS OS/2 environment using MS-C and MS-FORTRAN. RTACS(Real Time Advanced Control System), process control computer software for distributed or centralized architectures, is a package which meets functional requirements specified for typical continuous process applications like chemical processes. The package consists of 5 parts, which are DB(data base), OCF(Operator Console Functions), CL (Control logic Library), MSM(Multitasking and Scheduling, Manager) and UAI(User Applications Interface), based upon a table and function block architecture to improve the system performance.

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Development of Distributed Hydrological Analysis Tool for Future Climate Change Impacts Assessment of South Korea (전국 기후변화 영향평가를 위한 분포형 수문분석 툴 개발)

  • Kim, Seong Joon;Kim, Sang Ho;Joh, Hyung Kyung;Ahn, So Ra
    • Journal of The Korean Society of Agricultural Engineers
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    • v.57 no.2
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    • pp.15-26
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    • 2015
  • The purpose of this paper is to develop a software tool, PGA-CC (Projection of hydrology via Grid-based Assessment for Climate Change) to evaluate the present hydrologic cycle and the future watershed hydrology by climate change. PGA-CC is composed of grid-based input data pre-processing module, hydrologic cycle calculation module, output analysis module, and output data post-processing module. The grid-based hydrological model was coded by Fortran and compiled using Compaq Fortran 6.6c, and the Graphic User Interface was developed by using Visual C#. Other most elements viz. Table and Graph, and GIS functions were implemented by MapWindow. The applicability of PGA-CC was tested by assessing the future hydrology of South Korea by HadCM3 SRES B1 and A2 climate change scenarios. For the whole country, the tool successfully assessed the future hydrological components including input data and evapotranspiration, soil moisture, surface runoff, lateral flow, base flow etc. From the spatial outputs, we could understand the hydrological changes both seasonally and regionally.

Development of 0D Multizone Combustion Model and Its Coupling with 1D Cycle-Simulation Model for Medium-Sized Direct-Injection Diesel Engine (중형 직분식 디젤 엔진의 0-D Multi-zone 연소 모델 및 1-D Cycle Simulation 연계 기법 개발)

  • Choi, Seung-Mok;Min, Kyoung-Doug;Kim, Ki-Doo
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.34 no.6
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    • pp.615-622
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    • 2010
  • In this study, a 0D multizone spray-combustion model is developed for the estimation of the performance and NOx emission of medium-sized direct-injection marine diesel engine. The developed combustion model is coupled with the commercial 1D cycle-simulation model, Boost, to analyze the entire engine system, including the intake and exhaust. The combustion model code was generated using Fortran90, and the model was coupled with Boost by connecting the generated code to a user-defined high-pressure cycle (UDHPC) interface. Simulation was performed for two injectors (8 holes and 10 holes) and two engine loads (50% and 100%), and the results of simulation were in good agreement with engine performance test.