• Title/Summary/Keyword: Turning Stage

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Prediction of a research vessel manoeuvring using numerical PMM and free running tests

  • Tiwari, Kunal;Hariharan, K.;Rameesha, T.V.;Krishnankutty, P.
    • Ocean Systems Engineering
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    • v.10 no.3
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    • pp.333-357
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    • 2020
  • International Maritime Organisation (IMO) regulations insist on reduced emission of CO2, noxious and other environmentally dangerous gases from ship, which are usually let out while burning fossil fuel for running its propulsive machinery. Contrallability of ship during sailing has a direct implication on its course keeping and changing ability, and tries to have an optimised routing. Bad coursekeeping ability of a ship may lead to frequent use of rudder and resulting changes in the ship's drift angle. Consequently, it increases vessels resistance and also may lead to longer path for its journey due to zigzag movements. These adverse effects on the ship journey obviously lead to the increase in fuel consumption and higher emission. Hence, IMO has made it mandatory to evaluate the manoeuvring qualities of a ship at the designed stage itself. In this paper a numerical horizontal planar motion mechanism is simulated in CFD environment and from the force history, the hydrodynamic derivatives appearing in the manoeuvring equation of motion of a ship are estimated. These derivatives along with propeller thrust and rudder effects are used to simulate different standard manoeuvres of the vessel and check its parameters against the IMO requirements. The present study also simulates these manoeuvres by using numerical free running model for the same ship. The results obtained from both these studies are presented and discussed here.

Changes in the Enzyme Activities, Pectins and Structure of Persimmon Fruit during Softening (감과실의 연화중 효소활성, 펙틴 및 조직의 변화)

  • 신승렬;문광덕;이광희;김광수
    • Journal of the Korean Society of Food Science and Nutrition
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    • v.22 no.5
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    • pp.611-616
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    • 1993
  • This study was carried out to investigate change in the polygalacturonase and ${\beta}-galactosidase$ activities, pectins, cell wall structure of persimmon fruit during ripening and softening. Polygalacturonase and ${\beta}-galactosidase$ activities were not detected at turning stage. However polygalacturonase activities of mature and soft persimmon fruits were 55.01 and 206.70units/100g-fresh weight(fr. wt.), respectively. ${\beta}-Galactosidase$ activities of mature and soft persimmon fruits were 21.79 and 380.23unit/100g-fr. wt. respectively. The contents of total and insoluble pectins increased during maturation but decreased during softening. The content of water-soluble pectin increased during maturation and softening. The intercellular space was in larged during ripening, and middle lamella was degraded in mature persimmon fruit, and the cells of soft persimmon fruit were separated each other.

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Modeling of Deviation Angle and Pressure Loss Due to Rotor Tip Leakage Flow Effects in Axial Turbines (축류터빈에서 끝간격 유동에 의한 편향각과 압력손실의 모형)

  • Yoon, Eui Soo;Park, Moo Ryong;Chung, Myung Kyoon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.22 no.11
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    • pp.1591-1602
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    • 1998
  • Simple spanwise distribution models of deviation angle and pressure loss coefficient due to the tip leakage flow are formulated for use in association with the streamline curvature method as a flow analysis. Combining these new models with the previous deviation and loss models due to secondary flow, a robust streamline curvature method is established for flow analysis of single-stage, subsonic axial turbines with wide ranges of turning angle, aspect ratio and blading type. At the exit from rotor rows, the flow variables are mixed radially according to a spanwise transport equation. The proposed streamline curvature method is tested against a forced vortex type turbine as well as a free vortex type one. The results show that the spanwise variations of flow angle, axial velocity and loss coefficients at rotor exit are predicted with good accuracy, being comparable to a steady three-dimensional Navier-Stokes analysis. This simple and fast flow analysis is found to be very useful for the turbine design at the initial design phase.

A Study on the Steven Holl's Phenomenological Approaches in Architecture - Focused on the Phenomenological Characteristics of Nelson-Atkins Art Museum - (스티븐 홀의 현상학적 건축접근 방식에 관한 연구 - 넬슨-앳킨스 미술관에 적용된 내용을 중심으로 -)

  • Kim, Jun-Sung;Chung, Tae-Yong
    • Korean Institute of Interior Design Journal
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    • v.22 no.5
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    • pp.88-95
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    • 2013
  • The purpose of this study is to analyze the phenomenological approaches in Holl's architecture centered on his Nelson-Atkins Art Museum. This study mainly deals with concrete and practical architectural contents based on his recent works rather than existing studies about philosophical point of views to his architecture. Because Holl has had turning point from theoretical research to practical application and development stage. Therefore, this study aims to find out Holl's phenomenological approaches that were different from his early works. Nelson-Atkins art museum shows effect of luminosity as well as inflow of light in the phenomenological experiences of light and space. Holl gave new addition building that he designed contrasts of massing, transparency of material, colors to enhance existence of new building through phenomenological experiences. Narrow and long circulation and various focal points provide multi-view points and overlapped spaces in body experiences As a result, Holl shows shifts from theoretical application to architectural utilization. Nelson-Atkins art museum is important in that this project is one of stating points about this shift.

Landing Dynamic and Key Parameter Estimations of a Landing Mechanism to Asteroid with Soft Surface

  • Zhao, Zhijun;Zhao, JingDong;Liu, Hong
    • International Journal of Aeronautical and Space Sciences
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    • v.14 no.3
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    • pp.237-246
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    • 2013
  • It is of great significance to utilize a landing mechanism to explore an asteroid. A landing mechanism named ALISE (Asteroid Landing and In Situ Exploring) for asteroid with soft surface is presented. The landing dynamic in the first turning stage, which represents the landing performance of the landing mechanism, is built by a Lagrange equation. Three key parameters can be found influencing the landing performance: the retro-rocket thrust T, damping element damping $c_1$, and cardan element damping $c_2$. In this paper, the retro-rocket thrust T is solved with considering that the landing mechanism has no overturning in extreme landing conditions. The damping element damping c1 is solved by a simplified dynamic model. After solving the parameters T and $c_1$, the cardan element damping $c_2$ is calculated using the landing dynamic model, which is built by Lagrange equation. The validities of these three key parameters are tested by simulation. The results show a stable landing, when landing with the three estimated parameters T, $c_1$, and $c_2$. Therefore, the landing dynamic model and methods to estimate key parameters are reasonable, and are useful for guiding the design of the landing mechanism.

The Effect of Hull Appendages on Maneuverability of Naval Ship by Sensitivity Analysis (민감도 해석을 통한 선체 부가물이 함정의 조종성능에 미치는 영향 분석)

  • Kim, Dae Hyuk;Rhee, Key-Pyo;Kim, Nakwan
    • Journal of the Society of Naval Architects of Korea
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    • v.51 no.2
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    • pp.154-161
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    • 2014
  • Naval ships have hull appendages which are more exposed to the outside because of its small block coefficient compared with commercial ships. These exposed hull appendages like skeg, strut and shaft line affect the maneuverability of a ship. The effect of hull appendages has considered at initial design stage to estimate more accurate maneuverability. In this paper, sensitivity analysis is used to analyze the effect on maneuverability by hull appendages. 3 DOF maneuvering equations based on Mathematical Modelling Group (MMG) model are used and propeller & rudder model are modified to reflect the characteristics of twin propeller & twin rudder. Numerical maneuvering simulations (Turning test, Zig-zag test) for benchmark naval vessel, David Taylor Model Basin (DTMB) 5415 are performed. In every simulation, it is calculated that stability indices and maneuverability characteristics (Tactical Dia., Advance, 1st Overshoot, Time of complete cycle) with respect to the parameters (area times lift coefficient slope, attachment location) of hull appendages. As a result, two regression formulas are established. One is the relation of maneuverability characteristics and stability indices and the other is the relation of stability indices and hull appendages.

Modeling of Deviation Angle and Pressure Loss due to Rotor Tip Leakage Flow in Axial Turbines (축류터빈의 동익에서 끝간격 누설유동에 의한 편향각과 압력손실의 모형화)

  • 윤의수;오군섭;정명균
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1998.04a
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    • pp.13-13
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    • 1998
  • A simple model of the tip leakage flow models of the rotor downstream flow is developed, based on Lakshminarayana's theoretical concept on the tip clearance flow and the experimental data published in open literature. And new spanwise distribution models of deviation angle and pressure loss coefficient due to the tip leakage flow are formulated for use in association with the streamline curvature method as a through flow analysis. Combining these new models and previous deviation and loss models due to secondary flow, a robust streamline curvature method is established for flow analysis of single-stage, subsonic axial turbines with wide ranges of turning angle, aspect ratio and blading type. At the exit from rotor rows, the flow variables are mixed radially according to a spanwise transport equation. The proposed streamline curvature method is tested against a forced vortex type turbine as well as a free vortex type one. The results show that the spanwise variations of flow angle, axial velocity and loss coefficients at rotor exit are predicted with good accuracy, being comparable to a steady three-dimensional Navier-Stokes analysis. This simple and fast flow analysis is found to be very useful for the turbine design at the initial design phase.

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A Study on the Optimum Machining Conditions and Energy Efficiency of a Laser-Assisted Fillet Milling

  • Woo, Wan-Sik;Lee, Choon-Man
    • International Journal of Precision Engineering and Manufacturing-Green Technology
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    • v.5 no.5
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    • pp.593-604
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    • 2018
  • Laser-assisted machining (LAM) is known to be an effective and economical technique for improving the machinability of difficult-to-machine materials. In the LAM method, material is preheated using a laser heat source and then the preheated area is removed by following cutting tool. For laser-assisted turning (LAT), the configuration of the system is not complicated because laser irradiates from a fixed position. In contrast, laser-assisted milling (LAMill) system is not only complicated but also difficult to control because laser heat source must always move ahead of the cutting tool along a three dimensional (3D) tool path. LAMill is still early stage and cannot yet be used to machine finished products with 3D shapes. In this study, a laser-assisted fillet milling process was developed for machining 3D shapes. There are no prior studies combining fillet milling and LAMill. Laser-assisted fillet milling strategy was proposed, and effective depth of cut (EDOC) was obtained using thermal analysis. Experiments were designed using response surface method and cutting force prediction equations were developed using statistical analysis and regression analysis. The optimum machining conditions were also proposed, and energy efficiency of the LAMill was analyzed by comparing the specific cutting energy of conventional machining (CM) and LAMill.

Estimation of maneuverability of fisheries training vessel BAEK-KYUNG using numerical simulation method (수치 시뮬레이션 방법을 이용한 어업실습선 백경호의 조종성 추정)

  • KIM, Su-Hyung;LEE, Chun-Ki;LEE, Yoo-Won
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.57 no.3
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    • pp.246-255
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    • 2021
  • Most fishing vessels are less than 100 m in length (LBP), which is not mandatory for the IMO standards for ship maneuverability. Therefore, research on estimating the maneuverability of fishing vessel hull shapes are somewhat lacking compared to that of merchant ship hull shapes, and at the design stage, the numerical simulation method developed for merchant ships are applied without modification to estimate the maneuverability. Since this can cause estimation errors, the authors have derived a modified empirical formula that can improve the accuracy of estimating the maneuverability of fishing vessels in a previous study. In this study, using the modified empirical formula, the IMO maneuverability evaluation items, the turning motion test and Z-test simulations were performed on the fisheries training vessel BAEK-KYUNG and compared with the sea trial test result to verify the validity of the modified empirical formula. In conclusion, the modified empirical formula was able to estimate quantitatively and qualitatively similar to the result of the sea trial test. Such a study on estimating the maneuverability of fishing vessels will be a good indicator for fishing vessel operators and will help them analyze marine accidents.

Clinical application of Whidam's Su-Gi therapy to Low back pain (요통에 대한 휘담식 수기요법의 임상 적용)

  • Hun Mo Ahn;Sung Jin Chang;Han Joo Kang
    • Journal of Korean Medical Ki-Gong Academy
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    • v.21 no.1
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    • pp.13-21
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    • 2022
  • Objective : This report aimed to provide an introduction to the clinical application of Whidam's Su-Gi therapy to low back pain. Methods : Whidam's Su-Gi therapy for low back pain consisted of manual therapy according to upward and downward evaluations. Upward evaluation items include SLR, hip joint LOM, legs raising together, raising knee and turning left and right, and waist raising. Downward evaluation items include spinal alignment in sitting position, shoulder part tension, and cervical part tension. After performing the manual therapy according to the evaluation at each stage, the pain and dysfunction are reevaluated to confirm the negative and proceed to the next step. Conclusions : The clinical application of Whidam's Su-Gi therapy to low back pain is a method of interpreting and approaching low back pain disease with the theory of attraction pathology according to the principle of ChoGi-therapy(調氣療法).