• 제목/요약/키워드: Semi-empirical formula

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Study on slamming pressure calculation formula of plunging breaking wave on sloping sea dike

  • Yang, Xing
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제9권4호
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    • pp.439-445
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    • 2017
  • Plunging breaker slamming pressures on vertical or sloping sea dikes are one of the most severe and dangerous loads that sea dike structures can suffer. Many studies have investigated the impact forces caused by breaking waves for maritime structures including sea dikes and most predictions of the breaker forces are based on empirical or semi-empirical formulae calibrated from laboratory experiments. However, the wave breaking mechanism is complex and more research efforts are still needed to improve the accuracy in predicting breaker forces. This study proposes a semi-empirical formula, which is based on impulse-momentum relation, to calculate the slamming pressure due to plunging wave breaking on a sloping sea dike. Compared with some measured slamming pressure data in two literature, the calculation results by the new formula show reasonable agreements. Also, by analysing probability distribution function of wave heights, the proposed formula can be converted into a probabilistic expression form for convenience only.

정적압입 관통 실험을 이용한 복합재 적층판의 고속충격 탄도한계속도 예측 (Prediction of Ballistic Limit for Composite Laminates Subjected to High-velocity Impact Using Static Perforation Test)

  • 유원영;김인걸;이석제;김종헌
    • Composites Research
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    • 제26권1호
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    • pp.21-28
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    • 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.

CFD와 공간분포를 고려한 반경험식을 이용한 해머헤드 발사체의 천음속 압력섭동 예측 (Prediction of Pressure Fluctuations on Hammerhead Vehicle at Transonic Speeds Using CFD and Semi-empirical Formula Considering Spatial Distribution)

  • 김영화;남현재;김준모;선철
    • 한국항공우주학회지
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    • 제49권6호
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    • pp.457-464
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    • 2021
  • 위성발사체에 심각한 진동하중을 발생시키는 버펫 현상을 해석하기 위하여, CFD 해석과 반경험식을 결합하여 천음속 영역 해머헤드 발사체에서 발생할 수 있는 압력섭동을 예측하였다. RANS 해석을 수행하여 충격파 진동 영역, 박리영역, 박리 재부착 지점 등을 확인하였으며, 경계층 두께, 배제 두께, 경계층 끝단에서의 유동 정보를 계산하였다. RANS 결과와 공간 분포를 고려한 반경험식을 결합하여 해머헤드 페어링 주위의 압력 섭동과 파워스펙트럼을 예측하였고 시험 결과와 비교하였다.

Analysis of the Behavior of Bolt Jointed Wood Connections by Applying Semi-Rigid Theory

  • Kim, Gwang-Chul;Lee, Jun-Jae
    • Journal of the Korean Wood Science and Technology
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    • 제28권4호
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    • pp.72-82
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    • 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.

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Prediction of ship resistance in level ice based on empirical approach

  • Jeong, Seong-Yeob;Choi, Kyungsik;Kang, Kuk-Jin;Ha, Jung-Seok
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제9권6호
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    • pp.613-623
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    • 2017
  • A semi-empirical model to predict ship resistance in level ice based on Lindqvist's model is presented. This model assumes that contact between the ship and the ice is a case of symmetrical collision, and two contact cases are considered. Submersion force is calculated via Lindqvist's formula, and the crushing and breaking forces are determined by a concept of energy consideration during ship and ice impact. The effect of the contact coefficient is analyzed in the ice resistance prediction. To validate this model, the predicted results are compared with model test data of USCGC Healy and icebreaker Araon, and full-scale data of the icebreaker KV Svalbard. A relatively good agreement is achieved. As a result, the presented model is recommended for preliminary total resistance prediction in advance of the evaluation of the icebreaking performance of vessels.

쇄빙상선의 빙하중 추정식 고찰 (Ice Load Prediction Formulas for Icebreaking Cargo Vessels)

  • 최경식;정성엽
    • 대한조선학회논문집
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    • 제45권2호
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    • pp.175-185
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    • 2008
  • One of the concerns that arise during navigation in ice-covered waters is the magnitude of ice loads encountered by ships. However, the accurate estimation of ice loads still remains as a rather difficult task in the design of icebreaking vessels. This paper focuses on the development of simple ice load prediction formulas for the icebreaking cargo vessels. The maximum ice loads are expected from unbroken ice sheet and these loads are most likely to be concentrated at the bow area. Published ice load data for icebreaking vessels, from the model tests and also from full-scale sea trials, are collected and then several ice load prediction formulas are compared with these data. Finally, based on collected data, a semi-empirical ice load prediction formula is recommended for the icebreaking cargo vessels.

점 압력 스펙트럼에 대한 준-이론 모델을 사용한 효율적이고 정확한 평판 뒷전 소음의 예측 (Efficient and accurate prediction of flat plate trailing edge noise using semi-analytic model for point pressure spectra)

  • 이광세;정철웅
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2012년도 춘계학술대회 논문집
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    • pp.45-54
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    • 2012
  • In order to predict trailing edge noise from a flat plate more effectively and accurately, the prediction algorithm based on semi-analytic model for point pressure spectrum is proposed. The semi-analytic model consists of empirical models for point pressure spectra and theoretical model to determine the boundary layer characteristics needed for the empirical models. The proposed methods are applied to predict the trailing edge noise of the flat plate located in the mean flow of speed 38 m/s, for which the measured data are available. In present study, six empirical models for point pressure spectra are utilized for the predictions of trailing edge noise and their prediction results are compared to the measured data. Through the analysis of these comparisons, it is revealed that the present method based on non-frozen formula using Efimtsov model and Smol'yakov-Tkachenko model can provide more accurate and efficient predictions of trailing edge noise.

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점 압력 스펙트럼에 대한 준-이론 모델을 사용한 효율적이고 정확한 평판 뒷전 소음의 예측 (Efficient and Accurate Prediction of Flat Pate Trailing Edge Noise Using Semi-analytic Model for Point Pressure Spectra)

  • 이광세;정철웅
    • 한국소음진동공학회논문집
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    • 제22권6호
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    • pp.524-534
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    • 2012
  • In order to predict trailing edge noise from a flat plate more effectively and accurately, the prediction algorithm based on semi-analytic model for point pressure spectrum is proposed. The semi-analytic model consists of empirical models for point pressure spectra and theoretical model to determine the boundary layer characteristics needed for the empirical models. The proposed methods are applied to predict the trailing edge noise of the flat plate located in the mean flow of speed 38 m/s, for which the measured data are available. In present study, six empirical models for point pressure spectra are utilized for the predictions of trailing edge noise and their prediction results are compared to the measured data. Through the analysis of these comparisons, it is revealed that the present method based on non-frozen formula using Efimtsov model and Smol'yakov-Tkachenko model can provide more accurate and efficient predictions of trailing edge noise.

충돌분사의 충돌각 변화에 따른 난류특성의 실험적 연구 (An Experimental Study on the Turbulence Characteristics of a Cross Jet with Respect to Cross Angle Variations)

  • 노병준;최진철;강신재
    • 대한기계학회논문집
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    • 제13권5호
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    • pp.991-998
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    • 1989
  • 본 연구에서는 충돌각을 변수로 한 실험적 연구를 수행하기 위하여 여타의 변수를 고정하였으며, 유속은 R$_{e}$=5.2*$10^{4}$의 결과를 제시하였다.

Experimental study of internal solitary wave loads on the semi-submersible platform

  • Zhang, Jingjing;Liu, Yi;Chen, Ke;You, Yunxiang;Duan, Jinlong
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제13권1호
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    • pp.718-733
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    • 2021
  • A prediction method, based on the Morison equation as well as Froude-Krylov formula, is presented to simulate the loads acting on the columns and caissons of the semi-submersible platform induced by Internal Solitary Wave (ISW) respectively. Combined with the experimental results, empirical formulas of the drag and inertia coefficients in Morison equation can be determined as a function of the Keulegan-Carpenter (KC) number, Reynolds number (Re) and upper layer depth h1/h respectively. The experimental and calculated results are compared. And a good agreement is observed, which proves that the present prediction method can be used for analyzing the ISW-forces on the semi-submersible platform. Moreover, the results also demonstrate the layer thickness ratio has a significant effect upon the maximum horizontal forces on the columns and caissons, but both minimum horizontal and vertical forces are scarcely affected. In addition, the incoming wave directions may also contribute greatly to the values of horizontal forces exerted on the caissons, which can be ignored in the vertical force analysis.