• Explosives and Blasting
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• v.37 no.3
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• pp.1-12
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• 2019

The analysis methods of blast analysis models are classified into direct analysis and indirect analysis, and the latter is divided into semi-empirical and numerical analysis methods. In order to evaluate the applicability of the ELS blast analysis program, which is a program for analyzing the semi-empirical models, this study selected a simplified analytical model and examined the blast load characteristics of free-air burst explosion and surface burst explosion by using AT-Blast, RC-Blast, and Kinney and Graham's empirical equations, which are the semi-empirical analysis programs. As a result of analyzing the explosion pressure for the scaled distance and the incidence angle for the simplified analytical model, an appropriate analysis can be performed when the range of the scaled distance in the free-air burst explosion analysis was 0.3~0.461 and when the range of the scaled distance in the surface burst explosion analysis was 0.378~0.581. In terms of the incidence angle, the results analyzed within $45^{\circ}$ were considered to be appropriate.

• Journal of the Korean Chemical Society
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• v.26 no.4
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• pp.195-204
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• 1982

Semi-empirical MO calculations, EHT, CNDO/2, MINDO/3, and MNDO met hods, were performed on various geometries of n-butane, n-alkyl radical and tetramethylene diracal (triplet) in order to compare eigenvalue and eigenvector properties with those obtained by STO-3G method. All methods predicted the same relative order of stabilities of various geometries for n-butane; geometrical preferences were found to be dominated by one-electron factor, ${\pi}$-orbital energy changes being more impotant in the semi-empirical methods. The hyperconjugative energy changes accompanying structural changes from $(n-{\sigma}{\ast})_{trans}$ to (n-{\sigma}{\ast})cis were underestimated in the EHT, CNDO/2 and MINDO/3, whereas those were overestimated in the MNDO. The net destabilizing effect of $(n-{\sigma}{\ast})_{trans}$ structure was mainly due to the large internuclear energy involved in the structure. Through-space interaction between $n_1$ and $n_2$ orbitals of diradical caused energy gap narrowing of ${\Delta}E_{sp}$ and ${\Delta}{\varepsilon}={\varepsilon}_0$-${\varepsilon}_{av}$; through-space interaction had opposing effect to that of through-bond interaction. Due to the less severe neglect of differential overlaps in the MNDO, this energy gap narrowing effect appeared amplified in the MNDO. In general orbital properties were found to be reproduced satisfactorily, but eigenvalue properties were not, in all the semi-empirical methods especially when ${\sigma}-{\sigma}{\ast}$ and n-$n-{\sigma}{\ast}$interactions were involved.

• The Journal of the Acoustical Society of Korea
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• v.37 no.4
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• pp.163-173
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• 2018

This paper performed the prediction of the acoustic loads applied to the surface of the flight vehicle during flight. Acoustic loads during flight arise from the pressure fluctuations on the surface of body. The conventional method of predicting the acoustic loads in flight uses semi-empirical method derived from theoretical and experimental results. However, there is a limit in obtaining the flow characteristics and the boundary layer parameters of the flight vehicle which are used as the input values of the empirical equation through experiments. Therefore, in this paper, we use the hybrid method which combines the results of CFD (Computational Fluid Dynamics) with semi-empirical methods to predict the acoustic loads acting on flight vehicle during flight. For the flight vehicle with cone-cylinder-flare shape, acoustic loads were estimated for the subsonic, transonic, supersonic, and Max-q (Maximum dynamic pressure) condition flight. For the hybrid method, two kind of boundary layer edge estimation methods based on CFD results are compared and the acoustic loads prediction results were compared according to empirical equations presented by various researchers.

• Journal of the Korean Chemical Society
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• v.37 no.1
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• pp.62-67
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• 1993

The microscopic origin of nonlinear optical properties of quinoline derivatives have been investigated theoretically using MOPAC-AM1 method. In order to prepare promising nonlinear optical active polymers of polyquinoline derivatives, the optimized positions of strong electron donor and electron acceptor are determined in the heterocyclic ring for the energetically favorable structures. For each compound, the effect of the substituted positions on the microscopic nonlinear coefficients were investigated. Polyquinoline was already evaluated to have outstanding physical and mechanical properties so that its monomeric analogues were designed and synthesized for developing new second and third order nonlinear optical main chain polymers. Using the MOPAC-AM1 method, properties calculated include the intrinsic ground-state dipole moments, the polarizabilities, first and second hyperpolarizabilities under the condition of finite-field $(\omega$ = 0).

• Journal of the Korean Geotechnical Society
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• v.17 no.5
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• pp.43-50
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• 2001

딜라토메터는 실험의 간편성, 경제성, 신속성 및 반복성 등을 바탕으로 현장에서의 지반공학적 물성추정에 보편화되고 있다. 또한 간단한 장비구성과 손쉬운 사용법에도 불구하고 다양한 지반공학적 물성들 -예로서, $K_{o}$ , OCR, $c_{u}$ , $\psi$, $c_{h}$, $k_{h}$, ${\gamma}$, M, $u_{o}$ -을 추정할 수 있으며 다양한 지반공학적 설계문제에 성공적으로 적용되어 왔다. 그러나 제안된 관계식들이 대부분 기존실험 결과들과의 비교를 통하여 얻어진 경험적 상관관계이며, 특히 압밀계수 추정에 관한 부분은 관입시 평면변형 상태의 지반변형으로 인한 관입모사의 복잡성으로 인하여 피에조콘 소산시험 해석을 위해 제안된 이론 해들에 경험적인 가정사항들을 추가하여 사용하는 반경험적 방법들과 순수한 경험적인 방법이 사용되어 왔다. 본 연구에서는 elf라토메터 관입기의 실제 평면적을 등가의 원형반경으로 고려한 등가반경을 사용하고 최적화기법을 적용함으로써, 소산시험에서 실제 관측된 간극수압($p_2$)과 딜라토메터 소산시험을 모사하여 얻어진 예측 간극수압의 차이를 최소화하는 수평압밀계수 추정법을 제안하였다. 제안된 방법을 국내 양산지역에서 수행된 딜라토메터 소산실험에 적용하였으며 추정된 수평압밀계수 값을 기존의 딜라토메터 수평압밀계수 추정법들과 불교란 시료를 이용한 일차원 실내 압밀실험으로 얻어진 수평압밀계수 값들과 비교검증 하였다. 그 결과 제안된 방법으로 기존의 방법에 비해 실내 압밀실험 결과와 일치하는 수평압밀계수 추정결과를 얻었다. 또한, 제안된 방법으로 얻어진 수평압밀계수는 전 소산도 범위에서 고르게 관측값과 일치하는 소산곡선을 예측하여, 최적화기법을 이용한 딜라토메터 소산시험 해석으로 전 소산과정을 대표하는 압밀계수의 추정이 가능할 것으로 사료된다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.6
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• pp.457-464
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• 2021

To analyze the buffet phenomenon that causes serious vibration loads on a satellite launch vehicle, the pressure fluctuations on a hammerhead launch vehicle at transonic speeds are predicted by coupling CFD analysis and semi-empirical methods. From the RANS simulation, shock oscillation region, separation region, and separation reattachment region are identified, and the boundary layer thickness, the displacement thickness, and flow properties at boundary layer edge are calculated. The pressure fluctuations and power spectra on the hammerhead fairing are predicted by coupling RANS results and semi-empirical methods considering spatial distribution, and compared with the experimental data.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2007.12a
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• pp.176-178
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• 2007

부산신항 북컨테이너터미널 민차부두 1단계 공사에 적용된 안벽기초는 하부 대섬도 연약점토층 개량을 위한 SCP(Sand Compaction Pile) 개량층과 그 상부에 약 6m정도의 사석층으로 구성되어 있다. 안벽은 케이슨식으로 상부의 크레인 풍의 공용하중 작용시에 발생이 예상되는 안벽기초의 과도한 지반침하 방지를 위해 근고블럭에 의한 Preloading 공법이 적용되었다. 따라서, 프리로딩에 의한 하부기초지반의 침하관리가 중요 공사관리 포인트가 된다. 그러나, SCP층이나 사석총에 대한 침하량 예측은 반경험적 방법에 의존하기 때문에 실제와 상당한 차이가 발생하게 된다 본 연구에서는 사석층의 진동다짐에 의한 시공 특성을 반영하기 위해 굴착치환구간의 사석층에 대한 실측값을 이용하여 Terzaghi 변형식의 침하계수 a를 재산정하여 SCP개량구간에 적용함으로써 보다 합리적인 안벽기초의 침하량을 분석하였고 이를 사석층의 여성고 산정에 이용하였다.

• Journal of the Korean Chemical Society
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• v.30 no.2
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• pp.166-171
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• 1986

Hydrogen atom transfer reactions, $RNH_2+CH_3{\to}RNH+CH_4\;where\;R=H\;and\;CH_3$, were studied by MINDO/3 MO method. It is expected that stable complex may exist between $CH_3\;and\;NH_3$. Transition state characteristics and activation parameters including activation entropies have been determined. In cases of absolute and activation entropies, results are found to agree in general with ab initio and experimental values, wherever comparisions are possible.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.50 no.11
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• pp.755-762
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• 2022

The wind tunnel test data for the missile configuration were compared with analysis results using various semi-empirical code and CFD analysis code. The three types of configurations were used for comparison including 2 types of main wing, inline and interdigitate configuration that the main wing and tail intersect. Additionally, it was confirmed that the vortex flow was accurately predicted by comparing the CFD analysis result with the flow visualization test result.

• Journal of the Society of Naval Architects of Korea
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• v.35 no.4
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• pp.19-26
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• 1998

In this paper, we studied the Similar Ship(SS) concept[1,2] as a method to an experimental and semi-emperical approach for the estimation of hull hydrodynamic forces and hull-propeller-rudder interaction coefficients and used these methods to predict ship's manoeuvrability. The SS concept is adopted to use experimental data of prototype ships for manoeuvrability prediction of a new ship. The SS concept is composed of the key components as follows: existence of experimental data about prototype ship, availability of semi-emperical method for estimating the changes of hull force, a method to correct the prototype ship data. On the basis of these concepts, we attempted to simulate manoeuvrability at ballast and scantling draft conditions by making use of experimental data at full load draft condition and to simulate manoeuvrability of new ships by making use of experimental data for prototype. From present calculation, it was found that the present method can predict the ship's manoeuvrability accurately at early design stage.