• 제목/요약/키워드: impact testing

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개선된 충격해머의 동역학적 모델 (Improved dynamic model of the impact hammer)

  • 임병덕;최정현;허준혁
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.719-724
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    • 2002
  • Impact hammer is widely used as a convenient excitation tool in structural modal testing though, little is known about the dynamic characteristics of its impulse mechanism. Transmission of the impulsive force to the structure depends m the dynamic properties of the impact hammer as well as the stiffness of the tip. In this study an improved dynamic model of the impact hammer is proposed with the consideration of structure to be tested. The deformation masses of hammer tip and structure are as well as their contact stiffness. Numerical results show that this model is useful for the prediction of the impulse duration and the condition of rebounce..

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Bayesian Inference for Multinomial Group Testing

  • Heo, Tae-Young;Kim, Jong-Min
    • Communications for Statistical Applications and Methods
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    • 제14권1호
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    • pp.81-92
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    • 2007
  • This paper consider trinomial group testing concerned with classification of N given units into one of k disjoint categories. In this paper, we propose Bayesian inference for estimating individual category proportions using the trinomial group testing model proposed by Bar-Lev et al. (2005). We compared a relative efficience (RE) based on the mean squared error (MSE) of MLE and Bayes estimators with various prior information. The impact of different prior specifications on the estimates is also investigated using selected prior distribution. The impact of different priors on the Bayes estimates is modest when the sample size and group size we large.

Experimental and Numerical Simulation Studies of Low-Velocity Impact Responses on Sandwich Panels for a BIMODAL Tram

  • Lee, Jae-Youl;Shin, Kwang-Bok;Jeong, Jong-Cheol
    • Advanced Composite Materials
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    • 제18권1호
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    • pp.1-20
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    • 2009
  • This paper describes the results of experiments and numerical simulation studies on the impact and indentation damage created by low-velocity impact subjected onto honeycomb sandwich panels for application to the BIMODAL tram. The test panels were subjected to low-velocity impact loading using an instrumented testing machine at six energy levels. Contact force histories as a function of time were evaluated and compared. The extent of the damage and depth of the permanent indentation was measured quantitatively using a 3-dimensional scanner. An explicit finite element analysis based on LS-DYNA3D was focused on the introduction of a material damage model and numerical simulation of low-velocity impact responses on honeycomb sandwich panels. Extensive material testing was conducted to determine the input parameters for the metallic and composite face-sheet materials and the effective equivalent damage model for the orthotropic honeycomb core material. Good agreement was obtained between numerical and experimental results; in particular, the numerical simulation was able to predict impact damage area and the depth of indentation of honeycomb sandwich composite panels created by the impact loading.

충격햄머 실험에서 다자유도 주파수 응답스팩트럼의 개선 (An Enhancement of Multi-Dof Frequency Response Spectrum From Impact Hammer Testing)

  • 안세진;정의봉
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2002년도 추계학술대회논문집
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    • pp.623-629
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    • 2002
  • The spectrum of impulse response signal from an impulse hammer testing is widely used to obtain frequency response function(FRF) of the structure. However the FRFs obtained from impact hammer testing have not only leakage errors but also finite record length errors when the record length for the signal processing is not sufficiently long. The errors cannot be removed with the conventional signal analyzer which treats the signals as if they are always steady and periodic. Since the response signals generated by the impact hammer are transient and have damping, they are undoubtedly non-periodic. It is inevitable that the signals be acquired for limited recording time, which causes the finite record length error and the leakage error. In this paper, the errors in the frequency response function of multi degree of freedom system are formulated theoretically. And the method to remove these errors is also suggested. This method is based on the optimization technique. A numerical example of 3-dof model shows the validity of the proposed method.

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구조물의 안전진단을 위한 충격파의 주파수 영역 탐사에 관한 연구 (A study about frequency domain analysis of impact-wave for detecting of structural defects in the concrete structure)

  • 서백수;김훈;김형준;이상철
    • 한국지구물리탐사학회:학술대회논문집
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    • 한국지구물리탐사학회 2005년도 공동학술대회 논문집
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    • pp.165-180
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    • 2005
  • 충격탄성파 검사법은 콘크리트 구조물 내부의 결함과 외부 표면 사이에서 반사되어 전파되는 응력파를 이용한 비파괴 시험 방법이다. 본 연구에서 토목 구조물의 안전진단을 위하여 충격탄성파 검사법을 이용한 비파괴 시험을 수행하였다. 이를 위해서 토모그래피 방식을 이용한 투과법, 크로스 홀 방식을 이용한 투과법 그리고 일반적으로 터널라이닝과 같은 1차원 면에서 사용되는 반사법을 적용해 그 결과를 비교${\cdot}$분석하였다.

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CFRP 박육부재의 적층조건이 충격압궤특성에 미치는 영향 (Influence of Stacking Sequence Conditions on the Characteristics of Impact Collapse using CFRP Thin-Wall Structures)

  • 김영남;최효석;차천석;임광희;정종안;양인영
    • 대한기계학회논문집A
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    • 제24권12호
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    • pp.2945-2951
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    • 2000
  • Because of the inherent flexibility in their design for improved material properties, composites have wide applications in aerospace vehicles and automobiles. The purpose of this study is to investigate the energy absorption characteristics of CFRP( Carbon Fiber Reinforced Plastics); tubes on static and impact tests. Static compression tests have been carried out using the static testing machine(Shin-gang buckling testing machine)and impact compression tests have been carried out using the vertival crushing testing machine. When such tubes were subjected to crushing loads, the response is complex and depends on the interaction between the different mechanisms that control the crushing process. The collapse characteristics and energy absorption were examined. Trigger and interlaminar number affect energy absorption capability of CFRP tubes.

ESPI를 이용한 복합재료 박리결함의 정량평가 (Quantitative Evaluation of Delamination Inside of Composite Materials by ESPI)

  • 김경석;양광영;강기수;지창준
    • 비파괴검사학회지
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    • 제24권3호
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    • pp.246-252
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    • 2004
  • 복합재료는 이방성의 특징으로 매우 복잡한 역학거동을 하며, 해석 및 신뢰성 검사에 많은 어려움이 있다. 특히, 기존의 비파괴검사기법으로 내부손상을 검출하는 것은 매우 어려운 실정이다. 이에 본 연구에서는 복합재구조물의 가장 취약한 분야인 충격에 의한 손상이 발생할 경우 효과적인 검출기법을 개발하고, 충격에 따른 내부결함의 정량평가에 ESPI를 활용하였다. 인공결함을 이용하여 ESPI기법의 신뢰성을 확보하고 실제 충격손상 시험편에 대해 적용하여 5%이내의 오차율로 결함을 정량평가하였다.

충격햄머 실험에 의한 1자유도 주파수응답함수의 오차와 해결방법 (The Errors and Reducing Method in 1-dof Frequency Response Function from Impact Hammer Testing)

  • 안세진;정의봉
    • 한국소음진동공학회논문집
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    • 제12권9호
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    • pp.702-708
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    • 2002
  • The spectrum of impulse response signal from an impulse hammer testing is widely used to obtain frequency response function(FRF). However the FRFs obtained from impact hammer testing have not only leakage errors but also finite record length errors when the record length for the signal processing is not sufficiently long. The errors cannot be removed with the conventional signal analyzer which treats the signals as if they are always steady and periodic. Since the response signals generated by the impact hammer are transient and have damping, they are undoubtedly non-periodic. It is inevitable that the signals be acquired for limited recording time, which causes the errors. This paper makes clear the relation between the errors of FRF and the length of recording time. A new method is suggested to reduce the errors of FRF in this paper. Several numerical examples for 1-dof model are carried out to show the property of the errors and the validity of the proposed method.

횡방향 하중을 받는 CFRF 적층복합재의 내부손상에 관한 연구 (A Study on the Damage of CFRP Laminated Composites Under Out-of-Plane Load)

  • 김문생;박승범;오득창
    • 한국정밀공학회지
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    • 제12권11호
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    • pp.98-109
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    • 1995
  • An investigation was performed to study the inner damage of laminated composite plates subjected to out-of-plane load. During the investigation, inpact velocity and equivalent static load relationship was derived. Reddy's higher-order shear deformation theory(HSDT) and Hashin's failure criteria were used to determine inner stresses and damaged area. And impact testing was carried out on laminated composite plates by air gun type impact testing machine. The CFRP specimens were composed of [ .+-. 45 .deg. ]$_{4}$and [ .+-. 45 .deg. /0 .deg. /90 .deg. ]$_{2}$ stacking sequences with 0.75$^{t}$ * 26$^{w}$ * 100$^{l}$ (mm) dimension. After impact testing. As a result, a relationship holds between damaged area and impact energy, and a matrix cracking was caused by the interlaminar shear stress in the middle ply and was caused by the inplane transverse stress in the bottom ply.

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고분자 재료의 계장화 충격실험에 관한 연구 (Instrumented Impact Testing of Polymers)

  • 최선웅;우창기;윤종희
    • 한국공작기계학회논문집
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    • 제13권6호
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    • pp.23-28
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    • 2004
  • Impact behavior of polycarbonate in various defect state was investigated using an instrumented impact tester. A method of analyzing raw impact data was developed and successfully demonshsted the impact behavior in terms of load-displacement and energy-displacement curves. This technique was shown to be capable of separating defect no-defect initiated fractures as well as their propagation behaviors.