• Title/Summary/Keyword: Captive model test

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Prediction of Maneuverability of KCS Using Captive Model Test (구속모형시험을 이용한 KCS 선형의 조종성능 추정)

  • Shin, Hyun-Kyoung;Choi, Si-Hoon
    • Journal of the Society of Naval Architects of Korea
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    • v.48 no.5
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    • pp.465-472
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    • 2011
  • Recently, ultra large scale of ship is being ordered continuously and because of that, the accurate prediction of ship maneuverability in design stage becomes important matter. The model test like PMM test or CFD analysis are representative methods for predicting the maneuverability of ship. In this study, the captive model tests were carried out for predicting maneuverability of MOERI container ship(KCS) which is opened to the public using X-Y Carriage of Ocean Engineering Wide Tank of University of Ulsan. Considering the dimensions of tank, 2m class model ship was used for captive model test. CMT(Circular Motion Test) was performed for obtaining purer hydrodynamic coefficients related to yawing velocity. For getting hydrodynamic coefficients which cannot be obtained using CMT, PMM test(Planar Motion Mechanism test) were also performed. The maneuverability prediction results by simulation are compared with those of other research institutes.

Captive Model Test of Submerged Body Using CPMC (몰수체의 CPMC 구속모형시험)

  • Kim, Yeon-Gyu;Yun, Kun-Hang;Kim, Sun-Young;Kim, Dong-Jin
    • Journal of the Society of Naval Architects of Korea
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    • v.49 no.4
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    • pp.296-303
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    • 2012
  • The captive model test of submerged body using CPMC(Computerized Planar Motion Carriage) was carried out at the Ocean Basin of KORDI/MOERI. The target model is a submarine with general hullform. The forces and moments acting on the submerged body were measured by 6-axis waterproof gage. The oblique motion test and turning test were carried out in horizontal and vertical planes of the model. Maneuvering coefficients and derivatives were obtained from the test results. The stability indices in horizontal and vertical planes were obtained by using maneuvering derivatives. In this paper the introduction of test equipment and test results are presented.

Prediction of Maneuverability of KCS by CPMC Captive Model Test (CPMC 구속모형시험에 의한 KCS 선형의 조종성능 추정)

  • Kim, Yeon-Gyu;Yeo, Dong-Jin;Kim, Sun-Young;Yun, Kun-Hang;Oh, Byeong-Ik
    • Journal of the Society of Naval Architects of Korea
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    • v.46 no.6
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    • pp.553-561
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    • 2009
  • This paper presents the results of prediction of maneuverability of KCS by CPMC captive model test. The CPMC(Computerized Planar Motion Carriage) with captive model test equipment is installed at Ocean Engineering Tank of MOERI. KCS is the container ship which was open to the world by MOERI. And the test results for the prediction of maneuverability were presented by NMRI in Japan. The research results about the maneuverability of KCS were presented at SIMMAN 2008 Workshop in Denmark. The results of test and simulation of this paper are compared with the results of simulation by MOERI using test results of NMRI and simulation results by NMRI.

Prediction of Ship Manoeuvring Performance Based on Virtual Captive Model Tests (가상 구속모형시험을 이용한 선박 조종성능 평가)

  • Sung, Young Jae;Park, Sang-Hun
    • Journal of the Society of Naval Architects of Korea
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    • v.52 no.5
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    • pp.407-417
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    • 2015
  • For the more accurate prediction on manoeuvring performance of a ship at initial design phase, bare hull manoeuvring coefficients were estimated by RANS(Reynolds Averaged Navier-Stokes) based virtual captive model tests. Hydrodynamic forces and moment acting on the hull during static drift and harmonic oscillatory motions were computed with a commercial RANS code STAR-CCM+. Automatic and consistent mesh generation could be implemented by using macro functions of the code and user dependency could be greatly reduced. Computed forces and moments on KCS and KVLCC 1&2 were compared with the corresponding measurements from PMM(Planar Motion Mechanism) tests. Quite good agreement can be observed between the CFD and EFD results. Manoeuvring coefficients and IMO standard manoeuvres estimated from the computed data also showed reasonable agreement with those from the experimental data. Based on these results, we could confirm that the developed virtual captive manoeuvring model test process could be applied to evaluate manoeuvrability of a ship at the initial hull design phase.

A Study on the Captive Model Test of KCS in Regular Waves (KCS 선형의 규칙파 중 구속모형시험에 대한 연구)

  • Choi, Hujae;Kim, Dong Jin;Kim, Yeon Gyu;Yeo, Dong Jin;Yun, Kunhang;Lee, Gyeongjung
    • Journal of the Society of Naval Architects of Korea
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    • v.59 no.5
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    • pp.296-305
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    • 2022
  • In order to investigate maneuvering characteristics of KCS in waves, captive model test in regular waves was conducted. Purpose of the test is measuring maneuvering hull forces when ship is maneuvering in waves. Model test was carried out using CPMC (Computerized Planar Motion Carriage) of ocean engineering basin in KRISO (Korea Research Institute of Ships and Ocean engineering). Total 6 degrees-of-freedom motion were fixed by two points supporting captive model test device, which is specially designed for this test. This system estimates 6 degrees-of-freedom forces and moments through 12 strain gauge signals. Mapping matrix from strain gauge signals to 6 degrees-of-freedom forces and moments was derived by a well-organized calibration test. Static drift test was conducted in calm sea and in regular waves with various wave conditions. Hydrodynamic coefficients related to drift angle were extracted for each wave conditions, and the effect of waves on course stability was analyzed.

Changing Effect in Aerodynamic Characteristics of a Captive Body Separated from Aircraft (항공기 탑재체의 분리 후 공력 특성 변화 효과)

  • Cho, Hwan-Kee;Lee, Sang-Hyun;Kang, Chi-Hang
    • Journal of the Korea Institute of Military Science and Technology
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    • v.14 no.3
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    • pp.397-404
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    • 2011
  • The aerodynamic characteristics of a separated captive body in flow field around aircraft are studied to observe aerodynamic stability for safe separation from aircraft. Since the captive body separated from aircraft is initially exposed to unsteady flow pattern, the change of aerodynamic forces and moments should be measured to analyze how the flow pattern affects on the captive body at the vicinity of aircraft. Aerodynamic forces and moments of the separated captive body are measured at selected positions along predictable dropping trajectories. The measuring trajectories, generated by the free drop test of the dropping model in the wind tunnel, are consisted of 9 possible lines by free dropped trajectories. Experimental results show that the aerodynamic forces and moments are significantly varied with the distance between the captive body and aircraft. In conclusion, the change of aerodynamic characteristics within flow field around aircraft should be considered to simulate trajectories of the separated captive body from aircraft.

Prediction of Maneuverability of KCS with 4 Degrees of Freedom (KCS 선형의 4자유도 조종성능 추정)

  • Kim, Yeon-Gyu;Yeo, Dong-Jin;Son, Nam-Sun;Kim, Sun-Young;Yun, Kun-Hang;Oh, Byeong-Ik
    • Journal of the Society of Naval Architects of Korea
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    • v.48 no.3
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    • pp.267-274
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    • 2011
  • This paper presents the results of prediction of maneuverability of KCS about 4 degree of freedom(DOF) including roll motion. The prediction is carried out by CPMC captive model test. The CPMC(Computerized Planar Motion Carriage) with captive model test equipment including roll moment gage is installed at Ocean Engineering Tank of MOERI. KCS is the container ship open to the world by MOERI. To predict the 4 DOF maneuverability of a ship some tests with roll angle are conducted. And the prediction results of maneuverability by simulation are compared with the results of free running model test. The simulation results agree well with those of free running model tests.

Study of a Characteristics of Maneuvering Mathematical Model of Twin POD Cruise Ship (2축 POD 여객선의 조종운동 수학모형 특성 연구)

  • Kim, Yeon-Gyu;Yun, Kun-Hang;Kim, Sun-Young;Son, Nam-Sun
    • Journal of the Society of Naval Architects of Korea
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    • v.50 no.6
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    • pp.429-435
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    • 2013
  • Recently, to improve the safety and maneuverability at fairway around harbor the POD system has been equipped on a ship. And the interest about maneuvering characteristics of a cruise ship has been increasing. In this paper the mathematical model of maneuvering motion of a cruise ship with twin POD system in general speed and slow speed are presented. And the maneuvering coefficients of mathematical model are obtained from the captive model tests using CPMC(Computerized Planar Motion Carriage). Computer simulation using mathematical model in general speed and slow speed are carried out and compared with the results of free running model test with the same model ship. The differences between the mathematical models are compared and discussed. In this paper the mathematical models, the results of captive model test and simulation results are presented.

A Study on the Prediction Model of Unmanned Helicopter Fuel Consumption for the Captive Flight Test (탑재비행시험을 위한 무인헬기 연료 소모량 예측모형 연구)

  • Kim, Jisu
    • The Journal of the Korea Contents Association
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    • v.19 no.7
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    • pp.436-443
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    • 2019
  • The purpose of this paper is to establish a predictive model by analyzing the influence and correlation of factors affecting the fuel consumption of unmanned helicopters in Captive Flight Test. In this study, a four-factor two-level full factorial experiment was designed and tested using the design of experiments, results were analyzed to derive the main effects and interactions of the factors, and the predictive model was established through regression analysis. It is expected that the results from this study contribute to carrying out Captive Flight Test efficiently and the improvement of the test capability of Electronic Testing Range.

Maneuvering simulation of an X-plane submarine using computational fluid dynamics

  • Cho, Yong Jae;Seok, Woochan;Cheon, Ki-Hyeon;Rhee, Shin Hyung
    • International Journal of Naval Architecture and Ocean Engineering
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    • v.12 no.1
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    • pp.843-855
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    • 2020
  • X-plane submarines show better maneuverability as they have much longer span of control plane than that of cross plane submarines. In this study, captive model tests were conducted to evaluate the maneuverability of an X-plane submarine using Computational Fluid Dynamics (CFD) and a mathematical maneuvering model. For CFD analysis, SNUFOAM, CFD software specialized in naval hydrodynamics based on the open-source toolkit, OpenFOAM, was applied. A generic submarine Joubert BB2 was selected as a test model, which was modified by Maritime Research Institute Netherlands (MARIN). Captive model tests including propeller open water, resistance, self-propulsion, static drift, horizontal planar motion mechanism and vertical planar motion mechanism tests were carried out to obtain maneuvering coefficients of the submarine. Maneuvering simulations for turning circle tests were performed using the maneuvering coefficients obtained from the captive model tests. The simulated trajectory showed good agreement with that of free running model tests. From the results, it was proved that CFD simulations can be applicable to obtain reliable maneuvering coefficients for X-plane submarines.