• Journal of electromagnetic engineering and science
• /
• 제18권2호
• /
• pp.136-140
• /
• 2018

We propose an improved semi-empirical scattering model for X-band radar backscattering from rough sea surfaces. This new model has a wider validity range of wind speeds than does the existing semi-empirical sea spectrum (SESS) model. First, we retrieved the small-roughness parameters from the sea surfaces, which were numerically generated using the Pierson-Moskowitz spectrum and measurement datasets for various wind speeds. Then, we computed the backscattering coefficients of the small-roughness surfaces for various wind speeds using the integral equation method model. Finally, the large-roughness characteristics were taken into account by integrating the small-roughness backscattering coefficients multiplying them with the surface slope probability density function for all possible surface slopes. The new model includes a wind speed range below 3.46 m/s, which was not covered by the existing SESS model. The accuracy of the new model was verified with two measurement datasets for various wind speeds from 0.5 m/s to 14 m/s.

• 대한원격탐사학회지
• /
• 제17권2호
• /
• pp.141-153
• /
• 2001

A semi-empirical polarimetric backscattering model for bare soil surfaces is presented. Based on measurements by using polarimetric scatterometers and the JPL AirSAR, as well as the theoretical models, the backscattering coefficints $\sigma$$^0_w$, $\sigma$$^0_{hh}$ and $\sigma$$^0_{vh}$, and the parameters of the copolarized phase-difference probability density function, namely the degree of correlation $\alpha$ and the copolarized-phase-difference $\zeta$, are modeled empirically in terms of the volumetric soil moisture content m$_v$ and the surface roughness parameters $k_s$ and $k_l$, where k=2$\pi$f/c, s is the rms height and l is the correlation length.

• 화약ㆍ발파
• /
• 제37권3호
• /
• pp.1-12
• /
• 2019

폭발 해석 모델의 해석 방법은 직접적 해석과 간접적 해석으로 구별되며, 간접적 해석으로는 반경험적 해석 방법과 수치 해석적 방법으로 나뉜다. 본 연구에서는 반경험적 모델 해석의 프로그램인 ELS 폭발 해석 프로그램의 적용성을 평가하기 위해, 단순 해석 모델을 선정하고 다양한 반경험적 해석 프로그램인 AT-Blast, RC-Blast와 Kinney와 Graham의 경험식을 이용하여 자유 공중 폭발과 지표면 폭발에서의 폭발 하중 특성을 검토하였다. 단순 해석 모델에 대해 환산거리와 입사각에 대한 폭발 압력을 해석한 결과, 자유 공중 폭발 해석에서 환산거리의 범위는 $0.3{\sim}0.461m/kg^{1/3}$이고, 지표면 폭발 해석에서 환산거리의 범위는 $0.378{\sim}0.581m/kg^{1/3}$ 일 때 적합한 해석을 수행할 수 있으며, 입사각의 경우에는 $45^{\circ}$ 이내에서 해석한 결과가 적합한 것으로 판단된다.

• Journal of the Korean Wood Science and Technology
• /
• 제28권4호
• /
• pp.72-82
• /
• 2000

Attempts were made to analyze the behavior of single and multiple-bolted connections through theoretical methods such as European yield theory, empirical approaching method, and semi-rigid theory instead of many experimental methods that have been actually inefficient and non-economical. In the case of a single-bolted connection, if accurate characteristic values of a material could be guaranteed, it would be more convenient and economical to perform the behavior analysis using a model based on the semi-rigid theory, instead of the existing complex yield model, or the empirical formula which produces errors, giving different results from the actual ones. If the variables of equation determining the load and deformation could be appropriately controlled, the analytical method in conjunction with a semi-rigid theory could be effectively applied to obtain the desirably predicted value, considering that the appropriate solution could be derived through a simpler equation using a less difficult method compared to the existing yield model. It is concluded that analytical method with semi-rigid theory can be used in the behavior analysis of bolted connection because our developed method showed excellent analysis ability of behavior until number of bolt is two. Although our analytical method has the disadvantage that the number of bolt is limited to two, it is concluded that it has the advantage than numerical method which complicated and time-consuming.

• 대한원격탐사학회지
• /
• 제29권3호
• /
• pp.307-314
• /
• 2013

The Bidirectional Reflectance Distribution (BRD) effect is critical to interpret the surface information using remotely sensed data. This effect was caused by geometric relationship between sensor, target and solar that is inevitable effect for data of optical sensor. To remove the BRD effect, semi-empirical BRDF models are widely used. It is faster to calculate than physical models and demanded less observation than empirical models. In this study, Ross-Li kernel and Roujean kernel were used respectively in National Aeronautics and Space Administration (NASA) and European Organization for the Exploitation of Meteorological Satellites (EUMETSAT) that are used to compare each other. The semi-empirical model consists of three parts which are isotropic, geometric and volumetric scattering. Each part contained physical kernel and empirical coefficients that were calculated by statistical method. Red and NIR channel of SPOT/VEGETATION product were used to compute Nadir BRDF Adjusted Reflectance (NBAR) over East Asia area from January 2009 to December 2009. S1 product was provided by VITO that was conducted atmospheric correction using Simplified Method of Atmospheric Correction (SMAC). NBAR was calculated using corrected reflectance of red and NIR. Previous study has revealed that Roujean geometric kernel had unphysical values in large zenith angles. We extracted empirical coefficients in three parts and normalized reflectance to compare both BRDF models. Two points located forest in Korea peninsular and bare land in Gobi desert were selected for comparison. As results of time series analysis, both models showed similar reflectance change pattern and reasonable values. Whereas in case of empirical coefficients comparison, different changes pattern of values were showed in isotropic coefficients.

• Geomechanics and Engineering
• /
• 제30권1호
• /
• pp.11-26
• /
• 2022

One of the most important issues in tunneling, is the squeezing phenomenon. Squeezing can occur during excavation or after the construction of tunnels, which in both cases could lead to significant damages. Therefore, it is important to predict the squeezing and consider it in the early design stage of tunnel construction. Different empirical, semi-empirical and theoretical-analytical methods have been presented to determine the squeezing. Therefore, it is necessary to examine the ability of each of these methods and identify the best method among them. In this study, squeezing in a part of the Alborz service tunnel in Iran was estimated through a number of empirical, semi- empirical and theoretical-analytical methods. Among these methods, the most robust model was used to obtain a database including 300 data for training and 33 data for testing in order to develop a machine learning (ML) method. To this end, three ML models of Gaussian process regression (GPR), artificial neural network (ANN) and support vector regression (SVR) were trained and tested to propose a robust model to predict the squeezing phenomenon. A comparative analysis between the conventional and the ML methods utilized in this study showed that, the GPR model is the most robust model in the prediction of squeezing phenomenon. The sensitivity analysis of the input parameters using the mutual information test (MIT) method showed that, the most sensitive parameter on the squeezing phenomenon is the tangential strain (ε_θ^α) parameter with a sensitivity score of 2.18. Finally, the GPR model was recommended to predict the squeezing phenomenon in tunneling projects. This work's significance is that it can provide a good estimation of the squeezing phenomenon in tunneling projects, based on which geotechnical engineers can take the necessary actions to deal with it in the pre-construction designs.

• 한국항공우주학회지
• /
• 제36권3호
• /
• pp.220-228
• /
• 2008

반실험적 기법과 CFD 코드를 이용하여 자유회전 테일핀을 갖는 커나드 조종 미사일의 공력특성을 연구하였다. 반실험적 기법에서는 테일핀의 회전각에 따른 공력계수의 평균을 구한 후 자유회전 테일핀의 공력계수를 계산하였다. 또한 테일핀의 평균 롤링 및 롤 댐핑 모멘트계수를 이용하여 자유회전 테일핀의 회전율을 예측하였다. CFD 계산의 경우 중첩격자를 이용한 6-자유도 해석을 통해 테일핀의 회전율을 계산하였다. 미사일의 공력계수 예측 값들은 풍동실험 결과와 유사하게 나타났고, 커나드 롤 조종 및 요 조종시의 테일핀 회전율 또한 풍동실험결과와 근접하게 나타났다. 본 연구를 통해 자유회전 테일핀을 갖는 커나드 조종 미사일에 관한 공력해석에 반실험적 기법을 적용할 수 있음을 확인하였다.

• Composites Research
• /
• 제26권1호
• /
• pp.21-28
• /
• 2013

본 논문에서는 유효 면적의 제한이 있는 복합재 적층판의 탄도한계속도를 예측하였다. 탄도한계속도를 예측하기 위해 정적압입 관통실험과 고속충격 실험 그리고 준실험식을 이용하였다. 정적압입 관통실험을 통해 하중-변위 데이터를 취득하고 이를 이용해서 관통에너지를 측정하였다. 고속충격 실험을 통해 실제 관통 속도 및 관통 에너지를 측정하였다. 정적압입 관통실험과 고속충격 실험을 통해 구한 에너지를 이용해 준실험식을 만들고, 준실험식과 고속충돌 실험결과와 비교해 보았다. 위 방법을 이용해 탄도한계속도를 예측하였고 정적압입 관통 실험과 준실험식에 의한 탄도한계속도 예측의 타당성을 확인하였다.

• 한국시뮬레이션학회논문지
• /
• 제28권1호
• /
• pp.49-56
• /
• 2019

전산해석과 풍동시험을 이용하여 유도형 활공탄약의 공력특성을 연구하였다. 전산해석으로는 반실험적 기법인 Missile DATCOM과 전산유체역학 해석프로그램인 FLUENT를 사용하였다. 유도형 활공탄약에 대해 양력 및 항력, 피칭모멘트 등을 계산하여 기본적인 공력특성을 확인하였으며 기존의 탄약과는 전혀 다른 공력특성을 갖는 것을 확인했다. 전산해석을 통해 얻은 결과는 풍동시험을 통해 얻은 결과와 대체적으로 유사했다. 반실험적 기법으로 얻은 결과 중 피칭모멘트 값은 풍동시험결과와 약간 차이가 났지만, 전체적으로 전산해석의 결과는 시험결과와 유사한 경향과 값을 나타냈다. 본 연구를 통해 유도형 활공탄약의 공력특성을 확인하였으며, 유도형 활공탄약 초기설계 시 공력특성 분석을 위해 반실험적기법 및 전산유체역학적 해석 기법을 적용할 수 있음을 확인하였다.

• 항공우주시스템공학회지
• /
• 제16권3호
• /
• pp.1-9
• /
• 2022

본 연구에서는 MDO 프레임워크 개발을 위하여 다양한 준경험적 방법에 근거한 해석적 방법으로 경비행기인 창공-91의 비행운동 특성 파라미터를 추출하고 비행시험 방법을 기준으로 비교하여 평가하였다. 비교 대상의 준경험적 분석 방법은 Perkins 방법, McCormick 방법, 그리고 Smetana 방법이며, 각각의 방법을 통하여 주요 안정성/조종성 미계수와 동안정 계수를 산출하였다. 이에 대한 비교 기준은 비행시험을 수행하여 취득한 데이터로부터 출력오차방법을 활용하여 비행운동 미계수와 동안정 계수를 추출하였다. 아울러 경비행기의 비행특성을 우리나라 국토교통부의 항공기기술기준(KAS, Korean Airworthiness Standard)의 항목과 미 군용의 MIL-F-8785C의 기준으로 분석하여 평가하였다.