• Steel and Composite Structures
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• 제18권3호
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• pp.673-691
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• 2015

In this paper we are particularly focusing on the dynamic crack fatigue life of a 25 m length wind turbine blade. The blade consists of composite materiel (glass/epoxy). This work consisted initially to make a theoretical study, the turbine blade is modeled as a Timoshenko rotating beam and the analytical formulation is obtained. After applying boundary condition and loads, we have studied the stress, strain and displacement in order to determine the critical zone, also show the six first modes shapes to the wind turbine blade. Secondly was addressed to study the crack initiation in critical zone which based to finite element to give the results, then follow the evolution of the displacement, strain, stress and first six naturals frequencies a function as crack growth. In the experimental part the laminate plate specimen with two layers is tested under cyclic load in fully reversible tensile at ratio test (R = 0), the fast fracture occur phenomenon and the fatigue life are presented, the fatigue testing exerted in INSTRON 8801 machine. Finally which allows the knowledge their effect on the fatigue life, this residual change of dynamic behavior parameters can be used to predicted a crack size and diagnostic of blade.

• 한국소음진동공학회논문집
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• 제18권9호
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• pp.930-936
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• 2008

Fluid loading of a vibrating cylindrical shell has influence on natural frequencies and vibration magnitudes of the shell and the acoustic pressure of fluid. The vibroacoustics of fluid-filled cylindrical shells need the coupled solution of Helmholtz equation and governing equation of a cylindrical shell with boundary conditions. This paper proposed the wall impedance of fluid-filled axisymmetric cylindrical shells, focusing on the inner fluid/shell interaction. To propose the impedance, shell displacements used the linear combination of in vacuo shell modes. Acoustic pressure prediction of fluid used Kirchhoff-Helmholtz integral equation with Green's function of the plane mode. For the demonstration of the proposed results, numerical applications on mufflers were conducted.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2008년도 춘계학술대회논문집
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• pp.160-165
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• 2008

Fluid loading of a vibrating cylindrical shell can change natural frequencies and vibration magnitudes of the shell and a vibrating cylindrical shell can also change acoustic pressure of fluid. The vibroacoustics of fluid-filled cylindrical shells need the coupled solution of Helmholtz equation and governing equation of a cylindrical shell with boundary conditions. This paper proposed the wall impedance of fluid-filled axisymmetric cylindrical shells, focusing on the inner fluid/shell interaction. To propose the impedance, shell displacements used the linear combination of in vacuo shell modes. Acoustic pressure prediction of fluid used Kirchchoff-Helmholtz Integral equation with Green function of the plane mode. For the demonstration of the proposed results, numerical applications on mufflers were conducted.

• 한국해양공학회지
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• 제34권3호
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• pp.202-207
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• 2020

A track-type underwater construction robot (URI-R) was developed by the Korea Institute of Ocean Science & Technology. Because URI-R uses tracks to move on the seabed, insufficient ground strength may hinder its movement. For smooth operation of URI-R on the seabed, it is important to determine the geotechnical properties of the seabed. To determine these properties, standard penetration test (SPT), cone penetration test (CPT), and sampling are used on land. However, these tests cannot be applied on the seabed due to a high cost owing to the vessel, crane, sampler, and analysis time. To overcome these problems, a free fall cone penetration tester (FFCPT) is being developed. The FFCPT is a device that acquires the geotechnical properties during impact/penetration/finish phases by free fall in water. Depth information is crucial during soil data acquisition. As the FFCPT cannot measure the penetration depth directly, it is estimated indirectly using acceleration. The estimated penetration depth was verified by results of real tests conducted on land.

• Advances in aircraft and spacecraft science
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• 제6권6호
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• pp.497-513
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• 2019

A wind tunnel test was conducted that measured surface fluctuating pressures aft of a ramp at transonic speeds. Dynamic pressure test data was used to perform a study to determine best locations for streamwise sensor pairs for shocked and unshocked runs based on minimizing the error in root-mean-square acceleration response of the panel. For unshocked conditions, the upstream sensor is best placed at least 6.5 ramp heights downstream of the ramp, and the downstream sensor should be within 2 ramp heights from the upstream sensor. For shocked conditions, the upstream sensor should be between 1 and 7 ramp heights downstream of the shock, with the downstream sensor 2 to 3 ramp heights of the upstream sensor. The shock was found to prevent the passage coherent flow structures; therefore, it may be desired to use the shock to define the boundary of subzones for the purpose of loads definition. These recommendations should be generally applicable to a range of expansion corner geometries in transonic flow provided similar flow structures exist. The recommendations for shocked runs is more limited, relying on data from a single dataset with the shock located near the forward end of the region of interest.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2014년도 추계학술대회 논문집
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• pp.557-561
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• 2014

In this work, Altair Engineering's vibroacoustic modeling approach is used to simulate the acoustic signature of a simplified automobile in a wind tunnel. The modeling approach relies on a two step procedure involving simulation and extraction of acoustic sources using a high fidelity Computational Fluid Dynamics (CFD) simulation followed by propagation of the acoustic energy within the structure and passenger compartment using a structural dynamics solver. The tools necessary to complete this process are contained within Altair's HyperWorks CAE software suite. The CFD simulations are performed using AcuSolve and the structural simulations are performed using OptiStruct. This vibroacoustics simulation methodology relies on calculation of the acoustic sources from the flow solution computed by AcuSolve. The sources are based on Lighthill's analogy and are sampled directly on the acoustic mesh. Once the acoustic sources have been computed, they are transformed into the frequency domain using a Fast Fourier Transform (FFT) with advanced sampling and are subsequently used in the structural acoustics model. Although this approach does require the CFD solver to have knowledge of the acoustic simulation domain a priori, it avoids modeling errors introduced by evaluation of the acoustic source terms using dissimilar meshes and numerical methods. The aforementioned modeling approach is demonstrated on the Hyundai Simplified Model (HSM) geometry in this work. This geometry contains flow features that are representative of the dominant noise sources in a typical automobile design; namely vortex shedding from the passenger compartment A-pillar and bluff body shedding from the side view mirrors. The geometry also contains a thick poroelastic material on the interior that acts to reduce the acoustic noise. This material is modeled using a Biot material formulation during the structural acoustic simulation. Successful prediction of the acoustic noise within the HSM geometry serves to validate the vibroacoustic modeling approach for automotive applications.

• 한국산학기술학회논문지
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• 제21권10호
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• pp.16-22
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• 2020

한국해양과학기술원은 해저 표층지반의 특성을 원활하게 획득할 수 있는 자유낙하식 콘관입시험 시스템(Free-Fall Cone Penetration system, FFCPT)을 개발하고 있다. FFCPT를 통해 신호를 원활하게 획득하기 위해서는 전체 시험 시간동안 지속적으로 저장하는 방법 또는 사용자가 정의하는 시간 동안만 저장하는 방법이 고려될 수 있다. 효율적으로 데이터를 저장하고 관리하기 위해서는 사용자가 정의하는 시간 동안만 데이터를 저장하는 것이 유리하다. FFCPT는 낙하관성력을 최대한 확보하기 위해 회수용 와이어를 제외한 낙하에 방해되는 구성품이 최대한 배제되어 있다. 따라서 외부 보조장치를 활용한 데이터 저장 및 종료 시점 정의가 어렵다. 이에 FFCPT에 내부에 탑재된 센서를 통해 획득되는 신호를 이용하여 기본 거동을 분석하였고, 그 중 수심센서를 이용한 데이터 저장 시작과 종료를 인식할 수 있는 트리거 방식을 제안하였다. 수심 값의 3초와 0.03초 이동평균 차를 이용하여 낙하 시작 및 종료 시점을 판단하도록 하였다. 개발된 FFCPT를 이용하여 실해역 실험을 수행하였고, 트리거가 정상작동하여 원하는 데이터를 확보할 수 있었다.

• 한국산학기술학회논문지
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• 제22권3호
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• pp.352-361
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• 2021

한국해양과학기술원에서는 수중 공사용 구조물에 적용할 수 있는 수중 위치 인식 기술을 개발하고 있다. 정밀한 위치 인식을 위해 관성 항법을 기반으로 한 확장 칼만 필터를 사용하였으며, 비동기화 된 센서들의 데이터를 알고리즘 보정 단계에 적용하기 위하여 내부의 관측 행렬을 데이터에 따라 구분하여 업데이트 하였다. 수중 공사 환경, 설치 위치, 시스템 운용 편의성 등을 종합적으로 고려하여 수중 공사 구조물 하부에 붙여야 신호를 획득할 수 있는 Doppler velocity logger(DVL)는 설치 및 회수가 어렵기 때문에 이를 배제한 수중 공사 구조물 부착용 수중 위치 인식 복합 시험체를 제작하였으며 수조 환경에서 수중 위치 인식 성능 시험을 수행하였다. Ultra short-base line(USBL)로 측정된 수중 위치, 위치 벡터만 보정된 추정 위치, 그리고 위치와 속도 벡터를 보정한 추정 위치 결과를 원형 공산 오차(CEP)를 이용하여 비교 및 평가하였다. 그 결과 USBL 단독 위치 추정 CEP 0.02 m, 위치 벡터만 보정한 추정 위치 CEP 3.76 m., 위치 및 속도 벡터를 보정한 추정 위치 CEP 0.06 m로 평가되었다. 본 연구를 통해 DVL이 미적용된 비동기식 센서들을 이용하여 안정적인 수중 위치를 추정할 수 있음을 확인하였다.