• 제목/요약/키워드: Oscillatory Flow Regime

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FDDO를 이용한 실린더를 지나는 희박기체의 해석 (A Numerical Analysis of Rarefied Flow of Cylinder Using FDDO)

  • 안무영;장근식
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1998년도 춘계 학술대회논문집
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    • pp.138-144
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    • 1998
  • The BGK equation, which is the kinetic model equation of Boltzmann equation, is solved using FDDO(finite difference with the discrete-ordinate method) to compute the rarefied flow of monatomic gas. Using reduced velocity distribution and discrete ordinate method, the scalar equation is transformed into a system of hyperbolic equations. High resolution ENO(Essentially Non-Oscillatory) scheme based on Harten-Yee's MFA(Modified Flux Approach) method with Strang-type explicit time integration is applied to solve the system equations. The calculated results are well compared with the experimental density field of NACA0012 airfoil, validating the developed computer code. Next. the computed results of circular cylinder flow for various Knudsen numbers are compared with the DSMC(Direct Simulation Monte Carlo) results by Vogenitz et al. The present scheme is found to be useful and efficient far the analysis of two-dimensional rarefied gas flows, especially in the transitional flow regime, when compared with the DSMC method.

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마이크로 유동에서 플래핑 날개의 Tandem 모드를 이용한 추력향상에 대한 연구 (Thrust Enhancement through a Tandem Mode of Flapping Wing in Micro Flow)

  • 장성민;맹주성;안상준
    • 한국생산제조학회지
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    • 제20권5호
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    • pp.605-611
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    • 2011
  • In this study, based on previous studies, the thrust generated by using flapping tandem wings is examined. We studied on the relationship between the parameters for characterizing oscillatory tandem wings (namely, the Strouhal number and Reynolds number) for thrust generation in micro flow regime. At each Reynolds number, Strouhal number, heaving amplitude, distance between tandem wings, and phase difference are varied and the flapping motions of tandem mode are calculated to find the optimum conditions for generating thrust. As a result, comparing with a single flapping mode, we found that the minimum Strouhal number for generating thrust is shifted down up to approximately 25% when the tandem flapping mode is applied.

희석된 메탄/산소 대향류 확산화염에서 확산-열 불안정으로 인한 화염의 비선형 동적 거동에 관한 수치해석 (A Numerical Study on Nonlinear Dynamic Behavior of Diffusive-Thermal Instability in Diluted CH4/O2 Conterflow Diffusion Flames)

  • 손채훈
    • 대한기계학회논문집B
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    • 제28권6호
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    • pp.688-696
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    • 2004
  • Nonlinear dynamic behavior of diffusive-thermal instability in diluted CH$_4$/O$_2$ diffusion flames is numerically investigated by adopting detailed chemistry and transport. Counterflow diffusion flame is adopted as a model flamelet. Particular attention is focused on the pulsating-instability regime, which arises for Lewis numbers greater than unity, and the instability occurs at high strain rate near extinction condition in this flame configuration. Once a steady flame structure is obtained for a prescribed value of initial strain rate, transient solution of the flame is calculated after a finite amount of strain-rate perturbation is imposed on the steady flame. Transient evolution of the flame depends on the initial strain rate and the amount of perturbed strain rate. Basically, the dynamic behaviors can be classified into two types, namely non-oscillatory decaying solution and diverging solution leading to extinction. The peculiar oscillatory solution, which has been found in the previous study adopting one-step chemistry and constant Lewis numbers, is net observed in this study, which is attributed to both convective flow and preferential diffusion effects.

메탄/산소 대향류 확산화염에서 확산-열 불안정으로 인한 화염의 거동에 관한 수치적 연구 (Numerical Study on Dynamic Behavior of Diffusive-Thermal Instability in $CH_4/O_2$ Conterflow Diffusion Flames)

  • 손채훈
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2004년도 제28회 KOSCO SYMPOSIUM 논문집
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    • pp.95-101
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    • 2004
  • Dynamic behavior of diffusive-thermal instability in diluted $CH_4/O_2$ diffusion flames is numerically investigated by adopting detailed chemistry and transport. Counterflow diffusion flame is adopted as a model flamelet. Particular attention is focused on the pulsating-instability regime, which arises for Lewis numbers greater than unity, and the instability occurs at high strain rate near extinction condition in this flame configuration. Once a steady flame structure is obtained for a prescribed value of initial strain rate. transient solution of the flame is calculated after a finite amount of strain-rate perturbation is imposed Oil the steady flame. Transient evolution of the flame depends on the initial strain rate and the amount of perturbed strain rate. Basically, the dynamic behaviors can be classified into two types, namely non-oscillatory decaying solution and diverging solution leading to extinction. The peculiar oscillatory solution. which has been found in the previous study adopting one-step chemistry and constant Lewis numbers, is not observed in this study, which is attributed to both convective flow and preferential diffusion effects.

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주기적으로 회전진동하는 원주 후류의 Dynamic PIV 속도장 측정 (Dynamic PIV Measurements of Wake behind a Rotationally Oscillating Circular Cylinder)

  • 이정엽;이상준
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2007년도 추계학술대회
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    • pp.134-137
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    • 2007
  • The temporal evolution of wake behind a circular cylinder oscillating rotationally with a relatively high forcing frequency has been investigated experimentally using a dynamic PIV technique. Experiments were carried out with varying the frequency ratio $F_R\;(=f_f/f_n)$ in the range from 0.0 (stationary) to 1.6 at oscillation amplitude of ${\theta}_A=30^{\circ}$ and Reynolds number of $Re=4.14{\times}10^3$. Depending on the forcing condition ($F_R$), the flow was divided into three regimes; non-lock-on ($F_R=0.4$), transition ($F_R=0.8$, 1.6) and lock-on regimes ($F_R=1.0$) with markedly different flow structure in the near-wake region behind the cylinder. When the frequency ratio was less than 1.0 ($F_R{\le}1.0$), the rotational oscillatory motion of the cylinder decreased the length of the vortex formation region and enhanced the mutual interaction between large-scale vortices across the wake centerline. The entrainment of ambient fluid seemed to play an important role in controlling the near-wake flow and shear-layer instability. However, the flow characteristics changed markedly beyond the lock-on flow regime ($F_R=1.0$) due to high-frequency forcing. At $F_R=1.6$, the mutual interactions between the vortices shed from both sides of the cylinder were not so strong. Thereby, the flow entrainment and momentum transfer into the wake center region were reduced. In addition, the size of the large-scale vortices decreased since the lateral extent of the wake was suppressed.

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Effect of lock-on frequency on vortex shedding in the cylinder wake

  • Yoo Jung Yul;Sung Jaeyong;Kim Wontae
    • 한국가시화정보학회:학술대회논문집
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    • 한국가시화정보학회 2001년도 Proceedings of 2001 Korea-Japan Joint Seminar on Particle Image Velocimetry
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    • pp.86-99
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    • 2001
  • Vortex lock-on or resonance in the flow behind a circular cylinder is investigated from a time-resolved PIV when a single frequency oscillation is superimposed on the mean incident velocity. Measurements are made of the $K\acute{a}rm\acute{a}n$ and streamwise vortices in the wake-transition regime at the Reynolds number 360. Streamwise vortices at the lock-on and natural shedding states are observed, as well as the changes in the wake region with the change of the shedding frequency of lock-on state. When lock-on occurs, the vortex shedding frequency is found to be half the oscillation frequency as expected from previous experiments. At the lock-on state, the $K\acute{a}rm\acute{a}n$ vortices are observed to be more disordered by the increased strength and spanwise wavelength of the streamwise vortices, which leads to a strong three-dimensional motion. Recirculation and vortex formation region at the lock-on state is reduced as the oscillating frequency is increased. By comparing the Reynolds stresses at the lock-on and natural shedding states, $\bar{u'u'}\;and \;\bar{u'u'}$ at the lock-on state are concentrated on the shear layer around the cylinder. The $\bar{u'u'}\;at\;f_o/f_n=2.0$ has a large value near the centerline, compared with that of other cases. Considering the traces of maximum of u', in the wake region near the cylinder, wake width at the lock-on state is wider than that at the natural shedding state.

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감귤류 펙틴 용액의 리올리지 특성 (Rheological Properties of Citrus Pectin Solutions)

  • 황재관
    • 한국식품과학회지
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    • 제27권5호
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    • pp.799-806
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    • 1995
  • 고유점도가 3.75 dL/g인 감귤류 펙틴 용액의 전단점도 및 점탄성에 대한 농도의존성을 연구하였다. 전형적인 자수법칙 흐름 현상이 2.0% 이상의 펙틴 농도에서 관찰되었으며, 전단점도의 전단속도 의존성은 농도의 증가에 따라 더욱 뚜렷하게 나타났다. ${\eta}_{sp.o}$$C[\eta]$를 양대수 좌표에 그렸을 때 묽은 영역에서 진한 영역으로의 전이를 나타내는 $C^{*}[\eta]$는 약 4.0이었으며, 이때 ${\eta}_{sp.o}$의 값은 약 10.0을 나타내었다. 묽은 용액$(C[\eta]과 진한 용액$(C[\eta]>C^{*}[\eta])$에서 ${\eta}_{sp.o}$ $C[\eta]$의 기울기는 각각 1.1과 4.5였다. 전단점도를 ${\eta}/{\eta_0}$${\gamma}/{\gamma}_{0.8}$에 대하여 그렸을 때 $2{\sim}5%$의 농도에서는 잘 중첩되었으나, 6%의 고농도에서는 중첩곡선에서 벗어나는 현상을 보였다. 펙틴 용액의 점탄성을 조사한 결과 전 농도범위에서 손실탄성률$(G^{\prime\prime})$의 값이 저장탄성률$(G^\prime)$보다 훨씬 높은 값을 보여 점성이 전체 점탄성을 지배하는 것으로 나타났다. 저 농도에서 전단점도는 복소점도와 거의 비슷한 값을 보여 Cox-Merz 법칙에 잘 부합하였으나, 농도가 높아질수록 두 값은 차이를 보였다.

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