• 제목/요약/키워드: CTS 시험

검색결과 23건 처리시간 0.025초

로켓 부스터 분리 고속 풍동시험 (High-Speed Wind Tunnel Test on Rocket Booster Separation)

  • 라승호;김인선;옥호남;오범석;이준호
    • 한국항공우주학회지
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    • 제33권10호
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    • pp.75-81
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    • 2005
  • 낙하물 및 로켓 단분리 등과 같은 비행체 분리물의 궤적을 모사하기 위해 사출, 격자 및 CTS 시험과 같은 풍동시험 기법이 많이 사용된다. 본 논문에서는 3단형 과학로켓 개발 시 사용된 격자 및 CTS 시험 기법 및 대표적인 결과를 소개하였다. 시험에 사용된 풍동은 ONERA S2MA이며 마하수 2.0과 2.8에 대해 13개의 분리 궤적을 시험하였다. 시험 결과는 분리장치를 최적화기 위한 데이터베이스로 활용되었다.

모드 II 하중을 받는 CTS 시험편의 피로균열 전파거동에 관한 실험적 연구 (An Experimental Study on the Fatigue Crack Propagation Behavior in CTS Specimen under Mode II Loading)

  • 송삼홍;이정무
    • 대한기계학회논문집A
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    • 제27권7호
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    • pp.1217-1226
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    • 2003
  • The purpose of this paper is to investigate fatigue crack behavior under shear(Mode II) loading. Various specimens and devices have been used in order to produce Mode II loading in fatigue experiments for shear crack propagation. But, there is not sufficient comparisons of experimental results between Mode II and others loading modes, because of characteristics of applied loads and specimens. So, compact tension shear(CTS) specimens were used in this paper to investigate the propagation behavior of Mode II by comparing the experimental results between loading modes. We firstly observed the characteristics which was showed in Mode II experiment using CTS specimens. The experimental results under Mode II loading were compared with fatigue crack behavior under Mode I and Mixed-mode I+II loading. The characteristics for initiation and propagation behavior under Mode II loading was investigated by such comparisons.

CFD를 활용한 Flow Angularity 풍동시험기법의 외장분리 해석(1) (Store Separation Analysis of Flow Angularity Wind Tunnel Test Technique using CFD (1))

  • 손창현;서성은
    • 한국항공우주학회지
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    • 제45권1호
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    • pp.10-20
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    • 2017
  • 본 연구는 기존 Flow Angularity 장착물 분리 풍동시험 기법을 전산유체해석(Computational Fluid Dynamics)에 적용하여 해석 결과로부터 유동각 데이터베이스를 구성하고 6자유도 분리 궤적 해석한 결과를 전산유체해석의 CTS(Captive Trajectory Simulation) 해석 결과와 비교하여 CFD 해석 기법의 적용 가능성을 확인 한 것이다. Flow Angularity 기법의 전산유체해석 결과는 항공기와 외장간의 각 위치들에서 획득된 공력계수 데이터와 비교하여 데이터의 적절성을 확인하였다. 또한 Flow Angularity 기법으로 획득된 전산유체해석 데이터로부터 획득된 6자유도 외장 분리 궤적과 전산유체해석으로 해석한 CTS 외장분리 궤적을 비교하여 해석 기법의 적용 가능성을 확인하였다.

원공 결함을 갖는 CTS 시험편의 혼합모드 하중 하에서의 피로균열 전파거동 (Fatigue Crack Propagation Behavior in CTS Specimen Under Mixed-Mode Loading with Hole Defefects)

  • 송삼홍;신승만;이정무;서기정
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.137-142
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    • 2003
  • In this study, the propagation behavior of fatigue crack effected hole defects was investigated under mixed-mode I+II loading. To create mixed-mode stress field at crack tip, the compact tension shear (CTS) specimen and loading device were used in this tests. The propagation experiments of fatigue crack were performed by changing of the loading application angle(${\phi}$) and the distance(L) estimated from pre-crack tip to hole center located side by side by side with a pre-crack. As L changes, the variation for propagation aspect of fatigue crack, fatigue life and crack propagation rate were examined under mixed-mode loading. Under mixed-mode loading, the propagation rate of fatigue crack increased while the propagation direction changed dramatically because of the interference of hole defects.

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혼합모드 하중을 받는 CTS 시험편에서 $K_ I$,$K_ I1$ 와 J-적분의 측정방법 (Method to measure $K_ I$,$K_ I1$ and J-integral for CTS specimen under mixed mode loading)

  • 홍기주;강기주
    • 대한기계학회논문집A
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    • 제20권11호
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    • pp.3498-3506
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    • 1996
  • A loading device to be used in fracture experiment is presented. It's loading angle can be adjusted from $-45^{\circ}$ to $105^{\circ}$ at intervals of $15^{\circ}$ for a CTS ( compact tension-shear) specimen, so that it is to be useful to measure mixed mode toughness. The equations to give the $K_ I$, $K_ I1$ and J-integral for the experiment are evluated though finite elemetn analysis in which the loading procedure is simulated and the behaviors of the specimen such as load-displacement curve are estimated. In the course of the evaluation the values $K_ I$, $K_ I1$ and J-integral calculated through recentrly released numerical methods are employed as the reference ones.

외부 장착물 분리 해석을 위한 Off-line 6-DOF 시뮬레이션 프로그램 개발 (Development of an Off-line 6-DOF Simulation Program for Store Separation Analysis)

  • 곽인근;신재화;이승수;최기영;현재수;김남균
    • 한국항공우주학회지
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    • 제37권12호
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    • pp.1252-1257
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    • 2009
  • 항공기의 외부장착물 분리해석이 가능한 Off-line 6-DOF 시뮬레이션 프로그램을 개발 하였다. 개발한 프로그램은 풍동시험이나 CFD 해석을 통해 구축된 공력 데이터베이스를 이용하여 외부장착물의 분리 궤적을 예측할 수 있다. 공력 계수의 계산에는 flow angle 방법을 적용하였으며 분리 궤적 계산에는 사출력과 구속 조건의 적용이 가능하도록 하였다. 개발한 프로그램을 이용하여 군용항공기의 분리 궤적을 계산하였으며 이를 CTS 시험 결과와 비교하였다.

후판 용접부의 횡균열 발생 방지에 관한 연구(Ⅱ) (A Study on Prevention of Weld Transverse Crack for Thick Plate(Ⅱ))

  • 정호신;강성원
    • 한국해양공학회지
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    • 제13권3호통권33호
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    • pp.57-67
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    • 1999
  • Welding is widely applicable and reliable process and is mainly adopted for fabricating heavy structures. Recently, weld metal transverse cracks in butt and fillet weld joint is a serious problem, and they must be eliminated for improving weld joint reliability. The weld metal transverse crack susceptibility of butt and fillet joint was carried out by cantilever type tensile crack testing jig and CTS test. In this view of point, this study investigated the potential factors for weld metal transverse crack. The main results obtained were as follows: 1. The content o fdiffusible hydrogen in weld metal played an important role for weld metal transverse cracks. 2. From cantilever type tensile crack tests, it was pointed out that the higher the diffusible hydrogen content and tensile restraint, the more susceptible to weld metal transverse craking. 3. The TSN(thermal severity number) and diffusible hydrogen were important factors for determining weld metal transverse cracks in fillet weld joints.

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혼합모드 단일과대하중 하의 피로균열 전파거동에 관한 실험적 연구 (An Experimental Study on the Fatigue Crack Propagation Behavior Under Mixed-Mode Single Overload)

  • 송삼홍;이정무;홍석표
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.119-124
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    • 2003
  • In this study, retardation behavior of fatigue crack under single overloading of the mixed mode I+II state was experimentally investigated. To produce single overload in the mixed mode I+II state, the compact tension shear (CTS) specimen and loading device were used. The propagation tests for fatigue crack were performed under mode I loading overloading afterwards. We examined the observed deformation aspects, variation of fatigue life and crack propagation rate, and the aspects of retardation behavior from tests. The retardation effect of mixed-mode single overload on fatigue crack propagation behavior was smaller than that of mode I single overload. It has been confirmed that the retardation behavior did not immediately appear and the retardation length was short when the component of mixed-mode overload was changed.

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혼합모드 하중에서의 피로균열 전파거동 (Fatigue Crack Propagation Behavior under Mixed Mode Loading)

  • 송삼홍;이정무;최병호
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2000년도 추계학술대회 논문집
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    • pp.481-484
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    • 2000
  • Practical structures are subject not only to tension but also to shear and torsional loading. Even under uniaxial loading, when the load is not perpendicular to the crack plane, mixed mode crack can occur. Hence, it is necessary to evaluate the fatigue behavior under mixed mode loading. In this study, the propagation behavior of the fatigue crack of the STS304 steels under mixed mode loading condition was investigated. The mode I and II stress intensity factors of CTS specimen were calculated using elastic finite element method with experimental results. The fatigue crack propagation under mixed mode was evaluated by the effective stress intensity factor proposed by Tanaka.

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전단하중 하의 피로균열 전파거동의 특징 (The Characteristics of Fatigue Crack Propagation Behavior in Shear Load)

  • 이정무;송삼홍
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.302-307
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    • 2004
  • This paper reviewed characteristics of fatigue crack behavior observed by changing various shapes of initial crack and magnitudes of loading in compact tension shear(CTS) specimen subjected to shear loading. In the high-loading condition, fatigue crack under shear loading propagated branching from the pre-crack tip. Meanwhile, the secondary fatigue crack in the low-loading condition which was created in the notch root due to friction on the pre-crack face grew to a main crack. Influenced by the mode II loading condition, fatigue crack propagation retardation appeared in the initial propagation region due to the reduction of crack driving force and friction on crack face. In both cases, however, fatigue cracks grew in tensile mode type. Propagation path of fatigue crack under the shear loading was 70 degree angle from the initial crack regardless of its shape and load magnitude.

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