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UNCERTAINTY PROPAGATION ANALYSIS FOR YONGGWANG NUCLEAR UNIT 4 BY MCCARD/MASTER CORE ANALYSIS SYSTEM

  • Park, Ho Jin;Lee, Dong Hyuk;Shim, Hyung Jin;Kim, Chang Hyo
    • Nuclear Engineering and Technology
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    • v.46 no.3
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    • pp.291-298
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    • 2014
  • This paper concerns estimating uncertainties of the core neutronics design parameters of power reactors by direct sampling method (DSM) calculations based on the two-step McCARD/MASTER design system in which McCARD is used to generate the fuel assembly (FA) homogenized few group constants (FGCs) while MASTER is used to conduct the core neutronics design computation. It presents an extended application of the uncertainty propagation analysis method originally designed for uncertainty quantification of the FA FGCs as a way to produce the covariances between the FGCs of any pair of FAs comprising the core, or the covariance matrix of the FA FGCs required for random sampling of the FA FGCs input sets into direct sampling core calculations by MASTER. For illustrative purposes, the uncertainties of core design parameters such as the effective multiplication factor ($k_{eff}$), normalized FA power densities, power peaking factors, etc. for the beginning of life (BOL) core of Yonggwang nuclear unit 4 (YGN4) at the hot zero power and all rods out are estimated by the McCARD/MASTER-based DSM computations. The results are compared with those from the uncertainty propagation analysis method based on the McCARD-predicted sensitivity coefficients of nuclear design parameters and the cross section covariance data.

Improvement and application of DeCART/MUSAD for uncertainty analysis of HTGR neutronic parameters

  • Han, Tae Young;Lee, Hyun Chul;Cho, Jin Young;Jo, Chang Keun
    • Nuclear Engineering and Technology
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    • v.52 no.3
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    • pp.461-468
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    • 2020
  • The improvements of the DeCART/MUSAD code system for uncertainty analysis of HTGR neutronic parameters are presented in this paper. The function for quantifying an uncertainty of critical-spectrumweighted few group cross section was implemented using the generalized adjoint B1 equation solver. Though the changes between the infinite and critical spectra cause a considerable difference in the contribution by the graphite scattering cross section, it does not significantly affect the total uncertainty. To reduce the number of iterations of the generalized adjoint transport equation solver, the generalized adjoint B1 solution was used as the initial value for it and the number of iterations decreased to 50%. To reflect the implicit uncertainty, the correction factor was derived with the resonance integral. Moreover, an additional correction factor for the double heterogeneity was derived with the effective cross section of the DH region and it reduces the difference from the complete uncertainty. The code system was examined with the MHTGR-350 Ex.II-2 3D core benchmark. The keff uncertainty for Ex.II-2a with only the fresh fuel block was similar to that of the block and the uncertainty for Ex.II-2b with the fresh fuel and the burnt fuel blocks was smaller than that of the fresh fuel block.

THE ATMOSPHERE PARAMETERS AND THE LINE PROFILE VARIATIONS OF ρ PUPPIS

  • Yushchenko, A.V.;Dorokhova, T.N.;Gopka, V.F.;Kim, Chul-Hee;Lee, B.C.;Yushchenko, V.A.;Doikov, D.N.
    • Journal of The Korean Astronomical Society
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    • v.43 no.3
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    • pp.65-74
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    • 2010
  • We investigate ${\rho}$ Pup using the high resolution spectral observations taken from the VLT archive and observations at a 1.8m-Korean telescope with BOES spectrograph. The atmospheric parameters are determined using the iron-line abundance analysis. We derive an effective temperature value of $T_{eff}=6890{\pm}250K$, surface gravity of log g=$3.28{\pm}0.3$ dex, microturbulent velocity of ${\upsilon}_{micro}=4.1{\pm}0.4km\;s^{-1}$, and the iron abundance of log N=$7.82{\pm}0.15$. The projected rotational velocity of the star is close to ${\upsilon}$ sin i=3.5km $s^{-1}$. Asymmetric line profiles in the observed spectra and variation of this asymmetry with time show that both strong radial pulsation and weak non-radial pulsations are present in ${\rho}$ Pup.

Photofield-Effect in Amorphous InGaZnO TFTs

  • Fung, Tze-Ching;Chuang, Chiao-Shun;Mullins, Barry G.;Nomura, Kenji;Kamiya, Toshio;Shieh, Han-Ping David;Hosono, Hideo;Kanicki, Jerzy
    • 한국정보디스플레이학회:학술대회논문집
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    • 2008.10a
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    • pp.1208-1211
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    • 2008
  • We study the amorphous In-Ga-Zn-O thin-film transistors (TFTs) properties under monochromatic illumination ($\lambda=420nm$) with different intensity. TFT off-state drain current ($I_{DS_off}$) was found to increase with the light intensity while field effect mobility ($\mu_{eff}$) is almost unchanged; only small change was observed for sub-threshold swing (S). Due to photo-generated charge trapping, a negative threshold voltage ($V_{th}$) shift is also observed. The photofield-effect analysis suggests a highly efficient UV photocurrent conversion in a-IGZO TFT. Finally, a-IGZO mid-gap density-of-states (DOS) was extracted and is more than an order lower than reported value for a-Si:H, which can explain a good switching properties of the a-IGZO TFTs.

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Optimization of HIT Cell by Using Simulation -AFOS HET (시뮬레이션 실험을 통한 HIT Cell의 최적화 -AFOS HET)

  • Oh, Myoung-Seok;Heo, Jong-Kyu;Lee, Jun-Sin
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2008.11a
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    • pp.454-455
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    • 2008
  • 태양전지의 효율은 실리콘 자체의 특성에 의해서 결정 되거나 완성된 실리콘을 통해 태양전지를 제조하는 과정에서 웨이퍼의 두께와 도핑 농도의 조절을 통해 효율을 변화 시킬 수 있다. 높은 효율을 갖는 태양전지 설계를 위해 태양전지 시뮬레이터인 AFOS HET 프로그램을 이용하여 태양전지 웨이퍼 두께와 acceptor의 도핑 농도를 조절하였다. 최적화 결과 80nm ZnO, $300{\mu}m$ c-Si(p), 1nm a-Si(i), 1nm a-Si(n), $1{\mu}m$ Ag, acceptor의 도핑 농도 $7\times10^{16}cm^{-3}$ 에서 $V_{oc}$=697.7mV, $J_{sc}$=42.15mA/$cm^2$, $P_{max}$=0.0247W/$cm^2$, FF=83.51%, Eff=24.56%의 고효율을 얻을 수 있다. 본 연구를 통하여 태양전지 설계나 제조 시에 연구비를 절감할 수 있고 높은 효율의 태양전지로 접근할 수 있다.

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Wilson-Bappu effect : an indicator of stellar surface gravity

  • Park, Sun-Kyung;Lee, Jeong-Eun;Kang, Won-Seok;Lee, Sang-Gak
    • The Bulletin of The Korean Astronomical Society
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    • v.37 no.1
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    • pp.58.2-58.2
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    • 2012
  • Wilson and Bappu (1957), for the first time, and other precedent studies (Lutz & Kelker 1975; Pasquini et al. 1988; Dupree & Smith 1995; Wallerwstein et al. 1999; Pace et al. 2003) found a tight correlation (called Wilson-Bappu relationship - WBR) between stellar absolute visual magnitude and the width of the Ca II K line emission feature for late type stars. Here we re-visit WBR to claim that WBR can be an excellent indicator of stellar surface gravity of late type stars as well as a good indicator of distance. We have analyzed 103 high-resolution spectra of G, K and M type stars obtained by UVES and BOES by following the method by Pace et al. (2003) for measuring the widths of Ca II K lines(W). WBR found in our samples is Mv=33.26-17.79logW and the correlation is very tight. In this study, the stellar gravity(log g) has been derived using Kurucz ALAS9 model grid and MOOG code, which can determine $T_{eff}$ and [M/H] too.

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A study on the effect of residual stress on fatigue crack propagation rate of SS 41 material (SS 41材의 疲勞크랙 傳播速度에 미치는 熔接殘留應力의 影響에 관한 硏究)

  • Chung, Suk-Choo;Han, Byeong-Kee;Chung, Kang
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.12 no.3
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    • pp.473-480
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    • 1988
  • In this study, a method that can realize the effect of residual stresses on fatigue crack propagation has been proposed. This method requires that the relaxation quantities of residual stresses are measured by experimental method according to fatigue cycles and are employed to the experimental results of base materials by introducing the concept of superposition. SS41 material has been analyzed as an example. The results show that the relaxation factor of residual stresses for fatigue cycles is .alpha.$_{i}$= 1/0.6903+0.0380 $a_{I}$ the effective stress ratio for fatigue crack propagation length is ( $R_{eff}$)$_{i}$ = 1/1.1274+0.0118$_{I}$ and the fatigue crack propagation rate for relaxation quantities of residual stresses is (da/dN)$_{t}$ = 0.5 $K_{cf}$ - .DELTA.K/{1-1/1.1274+0.0118$_{ai}$ } $K_{cf}$ - .DELTA. K(da/dN), for stress ratio /R=0.5.io /R=0.5.5.

A study on prediction of stress intensity factor and fatigue crack growth behavior using the X-ray diffraction technique (X-선 회절을 이용한 피로균열진전거동과 응력확대계수 예측에 관한 연구)

  • Lim, Man-Bae;Kong, Yu-Sik;Boo, Myung-Hawn;Cha, Gee-Jun;Yoon, Han-Ki
    • Proceedings of the KSME Conference
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    • 2001.11a
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    • pp.317-323
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    • 2001
  • This study verified the relationship between fracture mechanics parameters$({\Delta}K,\;{\Delta}K_{eff},\;K_{max})$ and X-ray parameters $(\sigma_r,\;B)$ for SG365 steel at elevated temperature up to $300^{\circ}C$. The fatigue crack propagation test were carried out and X-ray diffraction technique according to crack length direction was applied to fatigue fractured surface. The residual stress on the fracture surface was found to increase low ${\Delta}K$ region, reach to a maximum value at a certain value of $K_{max}\;or\;{\Delta}K$ and then decrease. Residual stress were independent on stress ratio by arrangement of ${\Delta}K$ and half value breadth were independent by the arrangement of $K_{max}$. The equation of $\sigma_r-{\Delta}K$ was established by the experimental data. Therefore, fracture mechanics parameters could be estimated by the measurement of X-ray parameters.

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The Effect of Stress Ratio on the Surface Crack Growth Behavior in 7075-T651 Aluminum Alloy (7075-T651 Al合金의 表面균열進展에 미치는 應力比의 影響)

  • 박영조;김정규;신용승;김성민
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.10 no.1
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    • pp.62-69
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    • 1986
  • Fatigue surface crack growth was studied in 7075-T651 aluminum alloy plates subjected largely to bending loads. The surface crack length and its depth were measurement by the unloading elastic compliance method. The surface crack growth rate dc/dN, on the surface and da/dN, in the depth direction were obtained by the secant method. The stress intensity factor range .DELTA.K was computed by means of Newman and Raju equation. The aspect ratio a/c was presented in form of a/c=0.815-0.853(a/T). The effect of the stress ratio on the stable surface crack growth rates under increasing .DELTA.T is larger in lower .DELTA.K, while the relation between dc/dN, da/dN and the effective stress intensity factor range .DELTA.K$_{eff}$ is weakly dependent on the stress ratio.o.

Description of crack growth behavior of SB41 steel in terms of J integral (J적분에 의한 SB41강의 피로균열 진전 특성 평가)

  • 배원호;김상태;이택순
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.14 no.6
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    • pp.1568-1575
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    • 1990
  • Fatigue crack growth behavior was investigated in the center cracked plate of KS SB41 steel and the relation between the crack growth rate and various mechanical parameters was studied at small scale yielding, large scale yielding and full scale yielding. The crack opening ratio U was about 0.6-0.8 and had the larger value in the case of load control than that of strain control. Effective stress intensity factor range, .DELTA.K$_{eff}$ and J integral range, .DELTA.J were obtained from the notion of crack opening, and the crack growth rate was expressed with these values. The value of J integral range increased rapidly at stress ratio, R=0 in full scale yielding of load control test. COD value also increased rapidly with the increase of ligament net stress at large scale yielding of load control test.t.