• 제목/요약/키워드: Captive model test

검색결과 58건 처리시간 0.02초

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

  • 신현경;최시훈
    • 대한조선학회논문집
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    • 제48권5호
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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.

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

  • 김연규;윤근항;김선영;김동진
    • 대한조선학회논문집
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    • 제49권4호
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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.

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

  • 김연규;여동진;김선영;윤근항;오병익
    • 대한조선학회논문집
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    • 제46권6호
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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.

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

  • 성영재;박상훈
    • 대한조선학회논문집
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    • 제52권5호
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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.

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

  • 최후재;김동진;김연규;여동진;윤근항;이경중
    • 대한조선학회논문집
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    • 제59권5호
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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.

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

  • 조환기;이상현;강치행
    • 한국군사과학기술학회지
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    • 제14권3호
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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.

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

  • 김연규;여동진;손남선;김선영;윤근항;오병익
    • 대한조선학회논문집
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    • 제48권3호
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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.

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

  • 김연규;윤근항;김선영;손남선
    • 대한조선학회논문집
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    • 제50권6호
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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.

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

  • 김지수
    • 한국콘텐츠학회논문지
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    • 제19권7호
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    • pp.436-443
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    • 2019
  • 본 논문의 목적은 탑재비행시험 간 무인헬기 연료 소모량에 영향을 미치는 인자들의 영향정도와 상관관계를 분석하여 예측모형을 수립하는 것이다. 본 연구에서는 실험계획법을 활용하여 4인자 2수준 완전요인실험을 설계하여 실험을 수행하였고, 결과 값을 분석하여 인자들의 주 효과와 교호작용을 도출하고 회귀분석을 통해 예측모형을 수립하였다. 본 연구에서 도출한 결과를 활용하여 효율적인 탑재비행시험 및 전자시험장 시험 능력 향상에 기여할 것으로 기대된다.

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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    • 제12권1호
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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.