• 제목/요약/키워드: Critical Plane

검색결과 491건 처리시간 0.023초

내부유동을 포함한 굴곡된 파이프의 외평면 진동해석 (Out-of-Plane Vibrations of Angled Pipes Conveying Fluid)

  • Pak, chol-Hui;Hong, Sung-Chul;Kim, Tae-Ryong
    • Nuclear Engineering and Technology
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    • 제23권3호
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    • pp.306-315
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    • 1991
  • 본 연구는 두개의 직선 pipe가 elbow로 연결된 piping system의 내부에 유체가 흐를때 발생하는 out-of-plane 운동을 다루었으며, Extended Hamilton's principle을 이용하여 운동방정식을 유도하였다. clamped-clamped, clamped-pinned; pinned-pinned인 경계조건을 갖는 piping system의 경우, dynamic instability는 일어나지 않음을 고찰하였으며, 각 경계조건에 대한 진동수 방정식으로부터 고유진동수의 수치해를 얻었다. 유체의 속도와 Coriolis힘이 진동수에 미치는 영향을 고찰하였고, 유체의 속도와 압력이 어느값을 넘어설때 buckling-type instability가 일어남을 알았다. 그리고 유체의 속도와 압력의 함수로 등가임계속도를 정의하고 여러가지 경계조건에 대해 buckling 이 일어나는 등가임계속도를 계산하였다.

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Influence of interfacial adhesive on the failure mechanisms of truss core sandwich panels under in-plane compression

  • Zarei, Mohammad J.;Hatami, Shahabeddin;Gholami, Mohammad
    • Steel and Composite Structures
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    • 제44권4호
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    • pp.519-529
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    • 2022
  • Sandwich structures with the superior mechanical properties such as high stiffness and strength-to-weight ratio, good thermal insulation, and high energy absorption capacity are used today in aerospace, automotive, marine, and civil engineering industries. These structures are composed of moderately stiff, thin face sheets that withstand the majority of transverse and in-plane loads, separated by a thick, lightweight core that resists shear forces. In this research, the finite element technique is used to simulate a sandwich panel with a truss core under axial compressive stress using ABAQUS software. A review of past experimental studies shows that the bondline between the core and face sheets plays a vital role in the critical failure load. Therefore, this modeling analyzes the damage initiation modes and debonding between face sheet and core by cohesive surface contact with traction-separation model. According to the results obtained from the modeling, it can be observed that the adhesive stiffness has a significant influence on the critical failure load of the specimens. To achieve the full strength of the structure as a continuum, a lower limit is obtained for the adhesive stiffness. By providing this limit stiffness between the core and the panel face sheets, sudden failure of the structure can be prevented.

불규칙 접촉하중에서의 피로한도에 관한 연구 (Study on the fatigue Limit at Random Contact Loading)

  • 옥영구;안득만;조용주;이현우
    • 한국정밀공학회지
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    • 제19권8호
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    • pp.84-91
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    • 2002
  • This paper analyzes the subsurface stress at the spherical contact using Hamilton equation, and with that data, calculates the fatigue limit under the variations of friction coefficient using fatigue theory. After rough surface being made, this paper figures out the random load generated by contacting to the rough surface, analyzes the stress of its subsurface, and calculates the fatigue limit of the rough surface using fatigue theory. The three parts of the fatigue theory are applied, which are critical plane theory, stress invariant theory and mesoscopic theory.

접촉피로 파라미터의 개발 (Development of Fretting Fatigue Parameter)

  • 이혁재
    • 한국군사과학기술학회지
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    • 제14권1호
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    • pp.92-99
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    • 2011
  • In this study, new multi-axial, critical plane based, fretting fatigue crack initiation parameter is developed by the addition of a new term into the Modified Shear Stress Range(MSSR) parameter. The newly developed parameter (MSSR') is then used to evaluate fretting fatigue life of titanium alloy, Ti-6A1-4V with various contact conditions. Finite element analysis is also used in order to obtain stress distribution on the contact surface during fretting fatigue test, which is then used for the calculation of fretting fatigue parameter. The MSSR' parameter shows better performance in predicting fretting fatigue lives from the conventional fatigue data, and less scattering within fretting fatigue data with different contact geometries.

임무를 가지는 가스터빈 엔진 회전부품 피로수명 평가 (Mission based gas turbine engine rotating parts life evaluation)

  • 김경희;김현재;전승배;김동현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.385-390
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    • 2009
  • 가스터빈의 구조물은 열에 의한 응력과 기계적인 하중에 의한 응력이 동시에 중요하게 작용을 하며 다축응력상태에 놓이게 된다. 가스터빈 엔진은 일반적으로 임무를 가지게 되며 임무를 바탕으로 성능평가, 열전달해석, 구조해석, 수명평가의 일련의 과정을 거치게 된다. 임무에 따라 복잡하게 나타나는 변형율과 응력을 평가하기 위하여 임계평면법을 적용하였으며, 이를 바탕으로 보다 간단하고 편리한 평가 모델인 "The Simplified Model"을 개발하였다. 그리고 개발된 평가방법을 사용하여 터빈휠의 수명평가를 수행하여 결과를 나타내었다.

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지간적 직류Corona의 실질적 검토 (Experimental Study of DC Coronas in Point-to-Plane Short Gap)

  • 오철한;이성만
    • 대한전기학회논문지
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    • 제32권5호
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    • pp.157-163
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    • 1983
  • Positive and negative coronas in point-to-plane short gap have been investigated with the variations of point radius and gap length. Mainly the onset potentials and current pulses under various conditions were measured with a 70 MHz C.R.O. and a precise-controllable D.C. power supply. In the case of negative corona, the Trichel pulse corona, glow corona and spark regions were distinguished apparently and the critical gap lengths between them were also found clearly. In the case of positive corona, there are streamer corona, spark regions and the critical gap length between them, too. The current pulse forms of Trichel pulse corona of negative and streamer pulse corona of positive are similar in rising time, peak-to-peak time and pulse width. The glow corona current shows D.C. component in form.

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다축 피로 파라미터를 이용한 프레팅 피로 수명 예측에 관한 연구 (A study on fretting fatigue life prediction using multiaxial fatigue parameters)

  • 곽동현;노홍래;김진광;조상봉
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2006년도 춘계학술대회 논문집
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    • pp.359-360
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    • 2006
  • Recently, a lot of work and interest has been devoted to the development of multiaxial fatigue parameters for fretting fatigue life prediction. Many of these parameters have been reviewed in the literature for simple geometries like a cylinder-on-flat contact configuration. The purpose of this study was to estimate fretting fatigue life using critical plane approach which is one of the multiaxial fatigue theories.

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2상 주조 스테인리스강의 열화로 인한 2축 피로수명의 변화와 예측 (A Change and Prediction of Biaxial Fatigue Life of Cast Duplex Stainless Steels by Degradation)

  • 권재도;박중철
    • 대한기계학회논문집A
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    • 제28권4호
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    • pp.410-418
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    • 2004
  • The multiaxial fatigue test under in-phase and out-of$.$phase load were performed to study what degradation phenomenon affects fatigue life with virgin and 3600 hrs degraded materials. The various kind of fatigue data fur fatigue life prediction were acquired under pure axial and pure torsional load of fully reversal condition. The models which was investigated are: 1) the von Mises equivalent strain range, 2) the critical shear plane approach method of Fatemi-Socie(FS) parameter, 3) the modified Smith-Watson-Topper(SWT) parameter. The result showed that, fatigue life by material degradation are decreased and life prediction which was used the FS parameter is not conservative but the best result.

Dependence of superconductivity on the crystallinity of Nb films on Si wafers

  • Choi, Joonyoung;Kim, Chang-Duk;Jo, Younjung
    • 한국초전도ㆍ저온공학회논문지
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    • 제23권4호
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    • pp.1-5
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    • 2021
  • Among elemental metals, niobium (Nb) has the highest superconducting transition temperature (Tc) at ambient pressure. Thus, Nb films have been used in superconducting electronics and radio frequency cavity applications. In this study, the depositional factors determining the crystallinity and Tc of Nb films were investigated. An Nb film grown at a sputtering temperature of 240℃ exhibited the maximum crystallinity of Nb and the minimum crystallinity of niobium oxide. X-ray photoelectron spectroscopy confirmed a maximum atomic percent of niobium and a minimum atomic percent of oxygen. A sputtering power of 210 W and a sputtering time of 50 min were the optimal conditions for Nb deposition, and the Tc of the optimized film (9.08 K) was close to that of bulk Nb (9.25 K). Transmission electron microscopy images of the thick film directly confirmed the removal of the typical in-plane compressive strain in the (110) plane caused by residual stress.

미세홈 가공에 있어서 측면버 발생모델 (Side Burr Generation Model of Micro-Grooving)

  • 임한석;안중환
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1997년도 춘계학술대회 논문집
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    • pp.987-992
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    • 1997
  • Burrs always come out with the machining of ducterial with small size. Though the size of burrs is small, burrs dominate deterioration of the accuracy of the micro grooves. So the burr generation model especially side burr generation model was investigated to predict the size of the burrs at the given cutting conditions. The side shear plane is introduced to build the burr generation model and the width of side shear plane nomalized with cutting depth is defined with the shear angle. From the theoretical observation, the width of side shear plane can vary up 40% of the cutting depth. To determine the size of burr and stiffness, single groovings were carried out and it was found that there exist a critical depth of cut that the size or stiffness of the burr vary.

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