1,825 research outputs found

    The dynamics of transition to turbulence in plane Couette flow

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    In plane Couette flow, the incompressible fluid between two plane parallel walls is driven by the motion of those walls. The laminar solution, in which the streamwise velocity varies linearly in the wall-normal direction, is known to be linearly stable at all Reynolds numbers (ReRe). Yet, in both experiments and computations, turbulence is observed for Re360Re \gtrsim 360. In this article, we show that for certain {\it threshold} perturbations of the laminar flow, the flow approaches either steady or traveling wave solutions. These solutions exhibit some aspects of turbulence but are not fully turbulent even at Re=4000Re=4000. However, these solutions are linearly unstable and flows that evolve along their unstable directions become fully turbulent. The solution approached by a threshold perturbation could depend upon the nature of the perturbation. Surprisingly, the positive eigenvalue that corresponds to one family of solutions decreases in magnitude with increasing ReRe, with the rate of decrease given by ReαRe^{\alpha} with α0.46\alpha \approx -0.46

    Stable manifolds and homoclinic points near resonances in the restricted three-body problem

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    The restricted three-body problem describes the motion of a massless particle under the influence of two primaries of masses 1μ1-\mu and μ\mu that circle each other with period equal to 2π2\pi. For small μ\mu, a resonant periodic motion of the massless particle in the rotating frame can be described by relatively prime integers pp and qq, if its period around the heavier primary is approximately 2πp/q2\pi p/q, and by its approximate eccentricity ee. We give a method for the formal development of the stable and unstable manifolds associated with these resonant motions. We prove the validity of this formal development and the existence of homoclinic points in the resonant region. In the study of the Kirkwood gaps in the asteroid belt, the separatrices of the averaged equations of the restricted three-body problem are commonly used to derive analytical approximations to the boundaries of the resonances. We use the unaveraged equations to find values of asteroid eccentricity below which these approximations will not hold for the Kirkwood gaps with q/pq/p equal to 2/1, 7/3, 5/2, 3/1, and 4/1. Another application is to the existence of asymmetric librations in the exterior resonances. We give values of asteroid eccentricity below which asymmetric librations will not exist for the 1/7, 1/6, 1/5, 1/4, 1/3, and 1/2 resonances for any μ\mu however small. But if the eccentricity exceeds these thresholds, asymmetric librations will exist for μ\mu small enough in the unaveraged restricted three-body problem

    Travelling-waves consistent with turbulence-driven secondary flow in a square duct

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    We present numerically determined travelling-wave solutions for pressure-driven flow through a straight duct with a square cross-section. This family of solutions represents typical coherent structures (a staggered array of counter-rotating streamwise vortices and an associated low-speed streak) on each wall. Their streamwise average flow in the cross-sectional plane corresponds to an eight vortex pattern much alike the secondary flow found in the turbulent regime

    How do random Fibonacci sequences grow?

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    We study two kinds of random Fibonacci sequences defined by F1=F2=1F_1=F_2=1 and for n1n\ge 1, Fn+2=Fn+1±FnF_{n+2} = F_{n+1} \pm F_{n} (linear case) or Fn+2=Fn+1±FnF_{n+2} = |F_{n+1} \pm F_{n}| (non-linear case), where each sign is independent and either + with probability pp or - with probability 1p1-p (0<p10<p\le 1). Our main result is that the exponential growth of FnF_n for 0<p10<p\le 1 (linear case) or for 1/3p11/3\le p\le 1 (non-linear case) is almost surely given by 0logxdνα(x),\int_0^\infty \log x d\nu_\alpha (x), where α\alpha is an explicit function of pp depending on the case we consider, and να\nu_\alpha is an explicit probability distribution on \RR_+ defined inductively on Stern-Brocot intervals. In the non-linear case, the largest Lyapunov exponent is not an analytic function of pp, since we prove that it is equal to zero for 0<p1/30<p\le1/3. We also give some results about the variations of the largest Lyapunov exponent, and provide a formula for its derivative

    Linear stability analysis of resonant periodic motions in the restricted three-body problem

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    The equations of the restricted three-body problem describe the motion of a massless particle under the influence of two primaries of masses 1μ1-\mu and μ\mu, 0μ1/20\leq \mu \leq 1/2, that circle each other with period equal to 2π2\pi. When μ=0\mu=0, the problem admits orbits for the massless particle that are ellipses of eccentricity ee with the primary of mass 1 located at one of the focii. If the period is a rational multiple of 2π2\pi, denoted 2πp/q2\pi p/q, some of these orbits perturb to periodic motions for μ>0\mu > 0. For typical values of ee and p/qp/q, two resonant periodic motions are obtained for μ>0\mu > 0. We show that the characteristic multipliers of both these motions are given by expressions of the form 1±C(e,p,q)μ+O(μ)1\pm\sqrt{C(e,p,q)\mu}+O(\mu) in the limit μ0\mu\to 0. The coefficient C(e,p,q)C(e,p,q) is analytic in ee at e=0e=0 and C(e,p,q)=O(e^{\abs{p-q}}). The coefficients in front of e^{\abs{p-q}}, obtained when C(e,p,q)C(e,p,q) is expanded in powers of ee for the two resonant periodic motions, sum to zero. Typically, if one of the two resonant periodic motions is of elliptic type the other is of hyperbolic type. We give similar results for retrograde periodic motions and discuss periodic motions that nearly collide with the primary of mass 1μ1-\mu
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