• 한국해양공학회지
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• 제36권2호
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• pp.91-100
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• 2022

In general, the effect of roll motion is not considered in the study on maneuverability in calm water. However, for high-speed twin-screw ships such as the DTMB 5415, the coupling effects of roll and other motions should be considered. Therefore, in this study, the estimation of maneuverability using a 4-degree-of-freedom (DOF; surge, sway, roll, yaw) maneuvering mathematical group (MMG) model was conducted for the DTMB 5415, to improve the estimation accuracy of its maneuverability. Furthermore, a study on the change in turning performance according to the fin angle was conducted. To accurately calculate the lift and drag forces generated by the fins, it is necessary to consider the three-dimensional shape of the wing, submerged depth, and effect of interference with the hull. First, a maneuvering simulation model was developed based on the 4-DOF MMG mathematical model, and the lift force and moment generated by the side fins were considered as external force terms. By employing the CFD model, the lift and drag forces generated from the side fins during ship operation were calculated, and the results were adopted as the external force terms of the 4-DOF MMG mathematical model. A 35° turning simulation was conducted by altering the ship's speed and the angle of the side fins. Accordingly, it was confirmed that the MMG simulation model constructed with the lift force of the fins calculated through CFD can sufficiently estimate maneuverability. It was confirmed that the heel angle changes according to the fin angle during steady turning, and the turning performance changes accordingly. In addition, it was verified that the turning performance could be improved by increasing the heel angle in the outward turning direction using the side fin, and that the sway speed of the ship during turning can affect the turning performance. Hence, it is considered necessary to study the effect of the sway speed on the turning performance of a ship during turning.

• Steel and Composite Structures
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• 제22권2호
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• pp.399-409
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• 2016

The fracture propagation mechanism and fractured rock mass failure mechanism were important research in geotechnical engineering field. Many failures and instability in geotechnical engineering were related on fractures propagation, coalescence and interaction in rock mass under the external force. Most of the current research were limited to two-dimensional for the brittleness and transparency of three-dimensional fracture materials couldn't meet the requirements of the experiment. New materials with good transparent and brittleness were developed by authors. The making method of multi fracture specimens were established and made molds that could be reused. The tension-compression ratio of the material reached above 1/6 in normal temperature. Uniaxial and biaxial loading tests of single and double fracture specimens were carried out. Four new fractures were not found in the experiment of two-dimensional fractures such as the fin shaped crack, wrapping wing crack and petal crack and anti-wing crack. The relationship between stress and strain of the specimens were studied. The specimens with the load had experienced four stages of deformation and the process of the fracture propagation was clearly seen in each stage. The expansion characteristics of the fractured specimens were more obvious than the previous research.

• 제어로봇시스템학회논문지
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• 제16권4호
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• pp.329-334
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• 2010

This paper presents the design of a neural network based adaptive control for missile. Acceleration of missile by tail fin control cannot be controllable by DMI (Dynamic Model Inversion) directly because it is non-minimum phase system. To avoid the non-minimum phase system, dynamic model inversion is applied with output-redefinition method. In order to evaluate performance of the suggested controllers we selected the three cases such as control surface fail, control surface loss and wing loss for model uncertainty. The corresponding aerodynamic databases to the failure cases were calculated by using the Missile DATACOM. Using a high fidelity 6DOF simulation program of the missile the performance was evaluates.

• Wind and Structures
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• 제29권6호
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• pp.457-469
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• 2019

In this paper, a numerical solution is presented for supersonic flutter analysis of cantilever non-symmetric functionally graded (FG) sandwich plates. The plate is considered to be composed of two different functionally graded face sheets and an isotropic homogeneous core made of ceramic. Based on the first order shear deformation theory (FSDT) and linear piston theory, the set of governing equations and boundary conditions are derived. Dimensionless form of the governing equations and boundary conditions are derived and solved numerically using generalized differential quadrature method (GDQM) and critical velocity and flutter frequencies are calculated. For various values of the yaw angle, effect of different parameters like aspect ratio, thickness of the plate, power law indices and thickness of the core on the flutter boundaries are investigated. Numerical examples show that wings and tail fins with larger length and shorter width are more stable in supersonic flights. It is concluded for FG sandwich plates made of Al-Al₂O₃ that increase in volume fraction of ceramic (Al₂O₃) increases aeroelastic stability of the plate. Presented study confirms that improvement of aeroelastic behavior and weight of wings and tail fins of aircrafts are not consistent items. It is shown that value of the critical yaw angle depends on aspect ratio of the plate and other parameters including thickness and variation of properties have no considerable effect on it. Results of this paper can be used in design and analysis of wing and tail fin of supersonic airplanes.

• 한국발생생물학회지:발생과생식
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• 제13권2호
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• pp.115-122
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• 2009

기수산 2배체 일본재첩(Corbicula japonica)의 정자형성과정 및 정자의 미세 구조적 특징을 전자현미경 관찰에 의해 조사하였다. 세포학적 조사 결과, 기수산 2배체인 일본재첩의 정자 길이는 약 55${\mu}m$이다. 정자 두부(길이 약 12${\mu}m$)는 길게 신장되어 있으며 약간 구부러져 있다. 정핵 길이는 7.90 ${\mu}m$, 첨체 길이는 약 2.70 ${\mu}m$이다. 정자의 핵과 첨체의 형태는 각각 긴 화살 모양과 길다란 원추 모양을 나타낸다. 본 종(체외수정, 자웅이체, 난생종)의 정자 두부는 이미 몇몇 저자들에 의해서 보고된 3배체 재첩류(체내수정, 자웅동체, 난태생종)의 정자 두부에서 나타나는, 원시형으로부터 부분적으로 변형된 형태를 나타내고 있다. 그러나 부분적으로 변형된 2개의 편모가 있는 정자를 가지는 담수산 3배체인 자웅동체 조개류와 달리 한 개의 편모를 갖는 정자를 본 종은 생산한다. 2배체 일본재첩은 중심체를 둘러싸는 4개의 미토콘드리아를 가지고 있어, 짧은 중편을 가지는 다른 이매패류의 것들과 유사하다. 정자 미부 편모의 약소님은 중앙에 1쌍의 미세소관과 주변에 9쌍의 미세소관으로 구성되어 있다. 정자 미부의 악소님은 9+2구조를 가지며, 횡절단된 한 개의 편모를 갖는 정자에서 특히, 체외수정 어류들에서 나타는 날개 모야으이 악소님 lateral fin들이 관찰되었다.