• Title/Summary/Keyword: code validation

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CASMO-3/MASTER Pin Power Benchmarking for the B&W Critical Experiments

  • Kim, Kang-Seog;Song, Jae-Seung;Zee, Sung-Quun;Kim, Yong-Rae
    • Proceedings of the Korean Nuclear Society Conference
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    • 1996.05a
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    • pp.225-230
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    • 1996
  • A three-dimensional reactor core simulation code, MASTER has been developed as a part of ADONIS which is the Korean core design package in KAERI. CASMO-3 is used as a precedent lattice code for two-group microscopic cross section and heterogeneous formfunctions. The pin power reconstruction capability of CASMO-3/MASTER was evaluated for a validation and verification Five B&W critical experiments were selected as benchmark problems. These problems included two experiments for CE-type and three for WH-type fuel assemblies. Two of them contained gadolinia rods as burnable absorber. Comparison of the calculated pin power distributions with the measured ones demonstrate that CASMO-3/MASTER can predict the pin power distribution as well as CASMO-3/SIMULATE-3.

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Validation of electromagnetic physics models and electron range in Geant4 Brachytherapy application

  • A. Albqoor ;E. Ababneh ;S. Okoor;I. Zahran
    • Nuclear Engineering and Technology
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    • v.55 no.1
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    • pp.229-237
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    • 2023
  • The mechanics underlying photon and electron interactions was validated using our developed Brachytherapy computer code for high Dose Rate (HDR). By comparing the photon cross-section utilizing multiple physics libraries in the developed code, the results were benchmarked against experimental and theoretical findings. Klein-Nishina and experimental cross-section results were in good agreement with the Livermore library results. For two therapeutically relevant materials, the first scattered electron range was measured within 1 mm and 2 mm, which has significant implications for the interpretation of the kernel dose spikes observed in previous research.

QZSS TEC Estimation and Validation Over South Korea

  • Byung-Kyu Choi;Dong-Hyo Sohn;Junseok Hong;Woo Kyoung Lee
    • Journal of Positioning, Navigation, and Timing
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    • v.12 no.4
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    • pp.343-348
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    • 2023
  • The ionosphere acts as the largest error source in the Global Navigation Satellite System (GNSS) signal transmission. Ionospheric total electron content (TEC) is also easily affected by changes in the space environment, such as solar activity and geomagnetic storms. In this study, we analyze changes in the regional ionosphere using the Qusai-Zenith Satellite System (QZSS), a regional satellite navigation system. Observations from 9 GNSS stations in South Korea are used for estimating the QZSS TEC. In addition, the performance of QZSS TEC is analyzed with observations from day of year (DOY) 199 to 206, 2023. To verify the performance of our results, we compare the estimated QZSS TEC and CODE Global Ionosphere Map (GIM) at the same location. Our results are in good agreement with the GIM product provided by the CODE over this period, with an averaged difference of approximately 0.1 TECU and a root mean square (RMS) value of 2.89 TECU.

F-22의 개발과정(2)-선행 시제기에서 실용 시제기까지

  • Lee, Jong-Hui
    • Defense and Technology
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    • no.11 s.249
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    • pp.48-59
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    • 1999
  • 이 글은 미국의 차세대 전투기로 개발 및 시험중에 있는 F-22 항공기의 개발과정중 주요 형상변경을 비롯한 개발과정의 실제상황을 간접설명하기 위하여 록히드 항공사에서 발간한 "Code One" 잡지의 내용을 번역한 것이다. 본 내용은 미국의 항공 무기체계 개발 단계중 가장 설계 활동이 활발한 시범 및 입증단계(Demonstration/Validation Phase) 및 체계개발단계(Full Scale Development, or Engineering and Manufacturing Development Phase)의 설계 변경과정을 소개한 것이다. 독자의 이해를 돕기 위하여 미국의 항공무기체계 개발단계를 F-22 중심으로 간단히 소개하고자 한다

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Unsteady Compressible Flow past an Airfoil near the Moving Surface (파형 곡면 위를 비행하는 2차원 WIG익형의 비정상 압축성 유동 해석)

  • Im Y. H.;Chang K. S.
    • 한국전산유체공학회:학술대회논문집
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    • 1998.11a
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    • pp.191-196
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    • 1998
  • A two-dimensional airfoil flying over a wavy wall is calculated by solving the unsteady Euler equation. Unsteady Transonic flow over an NACA00012 airfoil in pitching motion has been computed for code validation. Some numerical results for NACA6409 airfoil under different wave number, wave length, fly height are presented. The numerical results show the variation of lift and pitching moment coefficients are increased as wave length decrease.

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Numerical Analysis about Optimal Conditions of GDICI Engine Operation using Intake Preheating (흡기가열을 이용한 가솔린압축착화 엔진의 최적구동조건에 관한 수치적 연구)

  • Choi, Mingi;Cha, Junepyo;Kwon, Seokjoo;Park, Sungwook
    • 한국연소학회:학술대회논문집
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    • 2012.04a
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    • pp.105-106
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    • 2012
  • This study is numerical analysis about optimal conditions of GDICI (gasoline direct injection compression ignition) engine operation using intake preheating. Numerical modeling was performed by using the KIVA-3V Release2 code integrated Chemkin chemistry solver II. For validation of numerical model, experiments were performed on a single-cylinder engine. Throughout the numerical simulations under variable conditions, the ranges of optimal conditions were found.

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Unsteady Performance Analysis of a Simple Shaft Gas Turbine Cycle (단순 가스터빈 사이클 과도 성능해석)

  • Kim, Soo-Yong;Soudarev, B.
    • 연구논문집
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    • s.30
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    • pp.5-13
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    • 2000
  • The computation scheme of simulating gas turbine transient behavior was developed. The basic principles of this scheme and main input data required are described. Calculation results are presented in terms of whole operating regime of the cycle. The influence of main initial parameters such as starting engine power, moment of inertia of the rotor, fuel supplying schedule etc. on performance characteristics of has turbine during transient operation is studied In addition, bleeding air influence on transient behavior was also considered For validation of the developed code, comparison of present calculation with that of measurement data of the experimental data for the range of operating period studied.

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Traceability Validation of Structured Behavioral Feature-Based Embedded SW Architecture Design Method (Structured Behavioral Feature기반 임베디드 SW 아키텍처 설계 방법의 추적성 검증)

  • Lee, Jung Tae;Jeong, Soyoung
    • Proceedings of the Korean Society of Computer Information Conference
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    • 2017.07a
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    • pp.281-284
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    • 2017
  • 최근 임베디드 시스템 개발이 Model Driven Engineering 방식으로 변화하면서 요구사항과 모델 간의 추적성을 보장하는 것이 매우 중요해졌다. 이 논문에서는 기존의 FDD(Feature Driven Development)와 FOSE(Feature Oriented Software Engineering) 방법론에 적용된 feature 개념을 재정의하여 이를 AUTOSAR platform에 적용하는 방법을 제시하며 요구사항부터 model, code까지 추적성을 검증한다.

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F-22의 개발과정 -선행 시제기에서 실용 시제기까지

  • Lee, Jong-Hui
    • Defense and Technology
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    • no.10 s.248
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    • pp.54-63
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    • 1999
  • 이 글은 미국의 차세대 전투기로 개발 및 시험중에 있는 F-22 항공기의 개발과정중 주요 협상변경을 비롯한 개발과정의 실제상황을 간접설명하기 위하여 록히드 항공사에서 발간한 "Code One" 잡지의 내용을 번역한 것이다. 본 내용은 미국의 항공 무기체계 개발 단계중 가장 설계 활동이 활발한 시범 및 입증단계(Demonstration/Validation Phase) 및 체계개발단계(Full Scale Development, or Engineering and Manufacturing Development Phase)의 설계 변경과정을 소개한 것이다. 독자의 이해를 돕기 위하여 미국의 항공 무기체계 개발단계를 F-22 중심으로 간단히 소개하고자 한다

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Satellite Remote Sensing of Groundwater: modeling, algorithm development and validation

  • Ghulam, Abduwasit;Qin, Qiming
    • Proceedings of the KSRS Conference
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    • 2003.11a
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    • pp.1383-1385
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    • 2003
  • Remote sensing has been widely used in the exploration of groundwater. In this paper, on the establishment of empirical function between ground water and soil moisture content 6S code is used to reduce uncertainties in the remote sensing of groundwater. Then ground water levels are calculated using 6S corrected and uncorrected ETM+ image along with isochronous meteorological information. Greater correspondence between field examined and satellite monitoring data is obtained from corrected image than from the uncorrected image.

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