319,530 research outputs found

    Resonant Interactions in Rotating Homogeneous Three-dimensional Turbulence

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    Direct numerical simulations of three-dimensional (3D) homogeneous turbulence under rapid rigid rotation are conducted to examine the predictions of resonant wave theory for both small Rossby number and large Reynolds number. The simulation results reveal that there is a clear inverse energy cascade to the large scales, as predicted by 2D Navier-Stokes equations for resonant interactions of slow modes. As the rotation rate increases, the vertically-averaged horizontal velocity field from 3D Navier-Stokes converges to the velocity field from 2D Navier-Stokes, as measured by the energy in their difference field. Likewise, the vertically-averaged vertical velocity from 3D Navier-Stokes converges to a solution of the 2D passive scalar equation. The energy flux directly into small wave numbers in the kz=0k_z=0 plane from non-resonant interactions decreases, while fast-mode energy concentrates closer to that plane. The simulations are consistent with an increasingly dominant role of resonant triads for more rapid rotation

    Comparison of the Geometrical Characters Inside Quark- and Gluon-jet Produced by Different Flavor Quarks

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    The characters of the angular distributions of quark jets and gluon jets with different flavors are carefully studied after introducing the cone angle of jets. The quark jets and gluon jets are identified from the 3-jet events which are produced by Monte Carlo simulation Jetset7.4 in e+e- collisions at s\sqrt s=91.2GeV. It turns out that the ranges of angular distributions of gluon jets are obviously wider than that of quark jets at the same energies. The average cone angles of gluon jets are much larger than that of quark jets. As the multiplicity or the transverse momentum increases, the cone-angle distribution without momentum weight of both the quark jet and gluon jet all increases, i.e the positive linear correlation are present, but the cone-angle distribution with momentum weight decreases at first, then increases when n > 4 or p_t > 2 GeV. The characters of cone angular distributions of gluon jets produced by quarks with different flavors are the same, while there are obvious differences for that of the quark jets with different flavors.Comment: 13 pages, 6 figures, to be published on the International Journal of Modern Physics

    Applications of diffraction theory to aeroacoustics

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    A review is given of the fundamentals of diffraction theory and the application of the theory to several problems of aircraft noise generation, propagation, and measurement. The general acoustic diffraction problem is defined and the governing equations set down. Diffraction phenomena are illustrated using the classical problem of the diffraction of a plane wave by a half-plane. Infinite series and geometric acoustic methods for solving diffraction problems are described. Four applications of diffraction theory are discussed: the selection of an appropriate shape for a microphone, the use of aircraft wings to shield the community from engine noise, the reflection of engine noise from an aircraft fuselage and the radiation of trailing edge noise

    Analysis of a Classical Matrix Preconditioning Algorithm

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    We study a classical iterative algorithm for balancing matrices in the LL_\infty norm via a scaling transformation. This algorithm, which goes back to Osborne and Parlett \& Reinsch in the 1960s, is implemented as a standard preconditioner in many numerical linear algebra packages. Surprisingly, despite its widespread use over several decades, no bounds were known on its rate of convergence. In this paper we prove that, for any irreducible n×nn\times n (real or complex) input matrix~AA, a natural variant of the algorithm converges in O(n3log(nρ/ε))O(n^3\log(n\rho/\varepsilon)) elementary balancing operations, where ρ\rho measures the initial imbalance of~AA and ε\varepsilon is the target imbalance of the output matrix. (The imbalance of~AA is maxilog(aiout/aiin)\max_i |\log(a_i^{\text{out}}/a_i^{\text{in}})|, where aiout,aiina_i^{\text{out}},a_i^{\text{in}} are the maximum entries in magnitude in the iith row and column respectively.) This bound is tight up to the logn\log n factor. A balancing operation scales the iith row and column so that their maximum entries are equal, and requires O(m/n)O(m/n) arithmetic operations on average, where mm is the number of non-zero elements in~AA. Thus the running time of the iterative algorithm is O~(n2m)\tilde{O}(n^2m). This is the first time bound of any kind on any variant of the Osborne-Parlett-Reinsch algorithm. We also prove a conjecture of Chen that characterizes those matrices for which the limit of the balancing process is independent of the order in which balancing operations are performed.Comment: The previous version (1) (see also STOC'15) handled UB ("unique balance") input matrices. In this version (2) we extend the work to handle all input matrice

    Low density expansion and isospin dependence of nuclear energy functional: comparison between relativistic and Skyrme models

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    In the present work we take the non relativistic limit of relativistic models and compare the obtained functionals with the usual Skyrme parametrization. Relativistic models with both constant couplings and with density dependent couplings are considered. While some models present very good results already at the lowest order in the density, models with non-linear terms only reproduce the energy functional if higher order terms are taken into account in the expansion.Comment: 16 pages,6 figures,5 table

    Quantum nonlocality of Heisenberg XX model with Site-dependent Coupling Strength

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    We show that the generalized Bell inequality is violated in the extended Heisenberg model when the temperature is below a threshold value. The threshold temperature values are obtained by constructing exact solutions of the model using the temperature-dependent correlation functions. The effect due to the presence of external magnetic field is also illustrated.Comment: 10 pages and 2 figures, published versio

    Constraints on kHz QPO models and stellar EOSs from SAX J1808.4-3658, Cyg X-2 and 4U 1820-30

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    We test the relativistic precession model (RPM) and the MHD Alfven wave oscillation model (AWOM) for the kHz QPOs by the sources with measured NS masses and twin kHz QPO frequencies. For RPM, the derived NS mass of Cyg X-2 (SAX J1808.4-3658 and 4U 1820-30) is 1.96 +/- 0.10 solar masses (2.83 +/- 0.04 solar masses and 1.85 +/- 0.02 solar masses), which is 30% (100% and 40%) higher than the measured result 1.5 +/- 0.3 solar masses (< 1.4 solar masses and 1.29 + 0.19 / - 0.07 solar masses). For AWOM, where the free parameter of model is the density of star, we infer the NS radii to be around 10 - 20 km for the above three sources, based on which we can infer the matter compositions inside NSs with the help of the equations of state (EOSs). In particular, for SAX J1808.4-3658, AWOM shows a lower mass density of its NS than those of the other known kHz QPO sources, with the radius range of 17 - 20 km, which excludes the strange quark matter inside its star.Comment: 6 pages, 3 figures, 2 table

    The Vector and Axial-Vector Charmonium-like States

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    After constructing all the tetraquark interpolating currents with JPC=1+,1,1++J^{PC}=1^{-+}, 1^{--}, 1^{++} and 1+1^{+-} in a systematic way, we investigate the two-point correlation functions to extract the masses of the charmonium-like states with QCD sum rule. For the 11^{--} qcqˉcˉqc\bar q\bar c charmonium-like state, mX=4.64.7m_X=4.6\sim4.7 GeV, which implies a possible tetraquark interpretation for the state Y(4660). The masses for both the 1++1^{++} qcqˉcˉqc\bar q\bar c and scsˉcˉsc\bar s\bar c charmonium-like states are around 4.04.24.0\sim 4.2 GeV, which are slightly above the mass of X(3872). For the 1+1^{-+} qcqˉcˉqc\bar q\bar c charmonium-like state, the extracted mass is 4.54.74.5\sim 4.7 GeV. We also discuss the possible decay modes and experimental search of the 1+1^{-+} charmonium-like states.Comment: 18 pages, 6 figures and 6 table
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