• 제목/요약/키워드: Trapezoidal Velocity

검색결과 67건 처리시간 0.023초

중공 및 중실소재를 이용한 스플라인 단조에 관한 연구 (Study on the Forging of Splines with Hollow and Solid Billets)

  • 조해용;최종웅;민규식
    • 한국정밀공학회지
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    • 제13권1호
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    • pp.108-115
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    • 1996
  • Forging of trapezoidal spline, serration and square spline with solid cylindrical billets and hollow one has been investigated by means of upper bound method. Kinematically admissible velocity fields for forging of splines have been proposed in this study. The half pitch of spline has been divided into several deformation regions. The neutral surface is introduced into forging of splines with flat punch and, for each step, it is assumed as a circle with its radius $r_n$. Upper bound solutions obtained by proposed kinematically admissible velocity fields are useful to predict the loads for forging of splines.

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Flutter characteristics of axially functional graded composite wing system

  • Prabhu, L.;Srinivas, J.
    • Advances in aircraft and spacecraft science
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    • 제7권4호
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    • pp.353-369
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    • 2020
  • This paper presents the flutter analysis and optimum design of axially functionally graded box beam cantilever wing section by considering various geometric and material parameters. The coupled dynamic equations of the continuous model of wing system in terms of material and cross-sectional properties are formulated based on extended Hamilton's principle. By expressing the lift and pitching moment in terms of plunge and pitch displacements, the resultant two continuous equations are simplified using Galerkin's reduced order model. The flutter velocity is predicted from the solution of resultant damped eigenvalue problem. Parametric studies are conducted to know the effects of geometric factors such as taper ratio, thickness, sweep angle as well as material volume fractions and functional grading index on the flutter velocity. A generalized surrogate model is constructed by training the radial basis function network with the parametric data. The optimized material and geometric parameters of the section are predicted by solving the constrained optimal problem using firefly metaheuristics algorithm that employs the developed surrogate model for the function evaluations. The trapezoidal hollow box beam section design with axial functional grading concept is illustrated with combination of aluminium alloy and aluminium with silicon carbide particulates. A good improvement in flutter velocity is noticed by the optimization.

Low velocity impact response and dynamic stresses of thick high order laminated composite truncated sandwich conical shell based on a new TDOF spring-mass-damper model considering structural damping

  • Azizi, A.;Khalili, S.M.R.;Fard, K. Malekzadeh
    • Steel and Composite Structures
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    • 제26권6호
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    • pp.771-791
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    • 2018
  • This paper deals with the low velocity impact response and dynamic stresses of composite sandwich truncated conical shells (STCS) with compressible or incompressible core. Impacts are assumed to occur normally over the top face-sheet and the interaction between the impactor and the structure is simulated using a new equivalent three-degree-of-freedom (TDOF) spring-mass-damper (SMD) model. The displacement fields of core and face sheets are considered by higher order and first order shear deformation theory (FSDT), respectively. Considering continuity boundary conditions between the layers, the motion equations are derived based on Hamilton's principal incorporating the curvature, in-plane stress of the core and the structural damping effects based on Kelvin-Voigt model. In order to obtain the contact force, the displacement histories and the dynamic stresses, the differential quadrature method (DQM) is used. The effects of different parameters such as number of the layers of the face sheets, boundary conditions, semi vertex angle of the cone, impact velocity of impactor, trapezoidal shape and in-plane stresses of the core are examined on the low velocity impact response of STCS. Comparison of the present results with those reported by other researchers, confirms the accuracy of the present method. Numerical results show that increasing the impact velocity of the impactor yields to increases in the maximum contact force and deflection, while the contact duration is decreased. In addition, the normal stresses induced in top layer are higher than bottom layer since the top layer is subjected to impact load. Furthermore, with considering structural damping, the contact force and dynamic deflection decrees.

Mechanism on suppression in vortex-induced vibration of bridge deck with long projecting slab with countermeasures

  • Zhou, Zhiyong;Yang, Ting;Ding, Quanshun;Ge, Yaojun
    • Wind and Structures
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    • 제20권5호
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    • pp.643-660
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    • 2015
  • The wind tunnel test of large-scale sectional model and computational fluid dynamics (CFD) are employed for the purpose of studying the aerodynamic appendices and mechanism on suppression for the vortex-induced vibration (VIV). This paper takes the HongKong-Zhuhai-Macao Bridge as an example to conduct the wind tunnel test of large-scale sectional model. The results of wind tunnel test show that it is the crash barrier that induces the vertical VIV. CFD numerical simulation results show that the distance between the curb and crash barrier is not long enough to accelerate the flow velocity between them, resulting in an approximate stagnation region forming behind those two, where the continuous vortex-shedding occurs, giving rise to the vertical VIV in the end. According to the above, 3 types of wind fairing (trapezoidal, airfoil and smaller airfoil) are proposed to accelerate the flow velocity between the crash barrier and curb in order to avoid the continuous vortex-shedding. Both of the CFD numerical simulation and the velocity field measurement show that the flow velocity of all the measuring points in case of the section with airfoil wind fairing, can be increased greatly compared to the results of original section, and the energy is reduced considerably at the natural frequency, indicating that the wind fairing do accelerate the flow velocity behind the crash barrier. Wind tunnel tests in case of the sections with three different countermeasures mentioned above are conducted and the results compared with the original section show that all the three different countermeasures can be used to control VIV to varying degrees.

階段式魚道에서 隔壁 形狀에 따른 水理學的 特性 및 魚類의 上流移動 (Hydraulic Characteristics and Upstream Migration of Fish by the Weir Type in a Pool-Weir Fishway)

  • 김진홍
    • 물과 미래
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    • 제29권6호
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    • pp.225-235
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    • 1996
  • 본 연구에서는 계단식어도의 격벽 형상에 따른 수리학적 특성과 어류의 상류이동에 미치는 효과를 다루고 있으며, 상류이동이 용이하도록 격벽의 적정 형태를 제시하는 것으로 하였다. 격벽 형상에 따른 수리학적 특성을 조사하고 적정 형태를 결정하기 위해 수리실험을 실시하였다. 실험결과 zig-zag 형태로 설치된 작은 notch를 가진 직사각형 격벽이 notch가 없는 단순 직사각형 격벽이나 사다리꼴 형태의 격벽보다 좋은 것이며이 밝혀졌는데, 이는 수위 저하시에도 어류의 상류이동이 가능하고 더우기 상류이동을 용이하게 하는 notch를 통한 낙하 흐름을 형성하기 때문인 것으로 판단되었다. Notch는 월류 최대유속이 어류의 유영한계유속을 넘지 않는 범위 내에서 표면류를 지속하도록, 즉 무차원유량 값이 0.27과 0.41 범위 내에 들도록 설계하는 것이 바람직한 것으로 나타났다.

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Asymmetric flows of non-Newtonian fluids in symmetric stenosed artery

  • Hun Jung;Park, Jong-Wook;Park, Chan-Guk
    • Korea-Australia Rheology Journal
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    • 제16권2호
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    • pp.101-108
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    • 2004
  • The hemodynamics behavior of the blood flow is influenced by the presence of the arterial stenosis. If the stenosis is present in an artery, normal blood flow is disturbed. In the present study, the characteristics of pulsatile flow in the blood vessel with stenosis are investigated by the finite volume method. For the validation of numerical model, the computation results are compared with the experimental ones of Ojha et al. in the case of 45% stenosis with a trapezoidal profile. Comparisons between the measured and the computed velocity profiles are favorable to our solutions. Finally, the effects of stenosis severity and wall shear stress are discussed in the present computational analysis. It can be seen, where the non-dimensional peak velocity is displayed for all the stenosis models at a given severity of stenosis, that it is exponentially increased. Although the stenosis and the boundary conditions are all symmetric, the asymmetric flow can be detected in the more than 57% stenosis. The instability by a three-dimensional symmetry-breaking leads to the asymmetric separation and the intense swirling motion downstream of the stenosis.

Anti-sway용 암을 가진 겐트리 크레인의 흔들림저감 제어 (Oscillation Motion Control of Gantry Crane System with Arm for Anti-Sway)

  • 김환성;박흥수;이동훈;박준형;김상봉
    • 동력기계공학회지
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    • 제2권1호
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    • pp.73-79
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    • 1998
  • In practical fields, the sway of crane systems leads to extra stress to the crane structure during the transporting operation and it is in close connection with its life. Usually, when we operate the cranes with high speed and manual control, the sway motion is irreducible. In this paper, a new type of crane system is proposed to avoid the irreducible sway of the crane systems. The proposed system is composed of mechanical arm with function of anti-sway based on conventional line system. By the anti-sway arm, we can realize to prevent the sway of the container box but cannot avoid the oscillation for the overall body of the crane. So, a controller design method to solve the above stated problem must be considered. The problem is solved by adopting the velocity pattern control methods of trapezoidal and curve types and its effectiveness is proved through experimental results.

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EOTS의 동적 안정성을 위한 속도 프로파일에 대한 연구 (Study of Speed Profile for Dynamic Stability of EOTS)

  • 이규찬;곽동기
    • 문화기술의 융합
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    • 제9권6호
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    • pp.919-925
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    • 2023
  • 현대의 드론에 장착되고 있는 임무 장비들의 소형화되고, 감시, 정찰 등의 여러 임무를 수행한다. 이에 따라 임무 장비는 풍하중, 모터 회전 등에 외란에 노출이 되어있으며, EOTS 구동에 있어 불안정성을 야기할 수 있다. 특히 EOTS의 시선의 위치 변경에 있어 단순 Step 입력은 급격한 속도의 변화를 일으켜 오버슈트를 발생시키며 여러 외란과 함께 불안정성을 야기할 수 있다. 따라서 EOTS의 시선의 변경을 할 시에 각속도가 사다리꼴 형태로 움직일 수 있도록 프로파일을 설정하고, 이를 이중 루프 제어기를 설계하여 위치 피드백을 받는 외부 루프의 Input에 적용 후 시스템의 안정성 비교와 최대 속도, 최대 가속도를 변화시키면서, 시스템이 안정적인 범위 내에서 속도 프로파일의 최적화를 연구하였다.

고속전철 판토그라프의 팬헤드 단면모델에 대한 공력특성 해석 (Aerodynamic Characteristics of Pantograph Panhead Sections in High Speed Railway)

  • 조운기;이종수
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2001년도 춘계학술대회논문집E
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    • pp.367-372
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    • 2001
  • The paper presents an improved way of aerodynamic quality in Korean Very High Speed Railway, The pantograph model being under development dissatisfies the required grade of aerodynamic lift force. So the present work proposes modified configurations of panheads to maintain consistent aerodynamic characteristics. Analysis has been performed using commercial CFD program. Simulation based analysis has been conducted with two different models. One is to attach the thin plate on the crossbar and the other is the use of trapezoidal cross section in contact strip. Various length of thin plate is simulated for flow velocity and acceptable value of plate length is selected which satisfy the necessary average lift force. Aerodynamic variation on the panheads strip is studied.

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리니어모터 이송 유연성 연삭가공 시스템에 관한 연구 (A study on the linear motor feed flexible disk grinding system)

  • 유송민
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2004년도 춘계학술대회 논문집
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    • pp.381-386
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    • 2004
  • A flexible disk grinding system process has been introduced that utilized varying disk orientation with respect to workpiece along with the applied feed speed. A known process model methodologies has been used to fomulate processed surface profiles. Various process conditions including cutting speed, maximum feed speed and orientation angles could applied to observe process outcomes. Even though continuous and constant feed speed has been applied to the process, the results from the trapezoidal input velocity profiles would be observed and compared. Based on the control strategies including neural network methodologies, several output results were compared to find the optimum process condition.

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