scholarly journals On scaling invariance and type-I singularities for the compressible Navier-Stokes equations

2019 ◽  
Vol 62 (11) ◽  
pp. 2271-2286 ◽  
Author(s):  
Zhen Lei ◽  
Zhouping Xin
2001 ◽  
Vol 434 ◽  
pp. 65-100 ◽  
Author(s):  
E. SERRE ◽  
E. CRESPO DEL ARCO ◽  
P. BONTOUX

Different instabilities of the boundary layer flows that appear in the cavity between stationary and rotating discs are investigated using three-dimensional direct numerical simulations. The influence of curvature and confinement is studied using two geometrical configurations: (i) a cylindrical cavity including the rotation axis and (ii) an annular cavity radially confined by a shaft and a shroud. The numerical computations are based on a pseudo-spectral Chebyshev–Fourier method for solving the incompressible Navier–Stokes equations written in primitive variables. The high level accuracy of the spectral methods is imperative for the investigation of such instability structures. The basic flow is steady and of the Batchelor type. At a critical rotation rate, stationary axisymmetric and/or three-dimensional structures appear in the Bödewadt and Ekman layers while at higher rotation rates a second transition to unsteady flow is observed. All features of the transitions are documented. A comparison of the wavenumbers, frequencies, and phase velocities of the instabilities with available theoretical and experimental results shows that both type II (or A) and type I (or B) instabilities appear, depending on flow and geometric control parameters. Interesting patterns exhibiting the coexistence of circular and spiral waves are found under certain conditions.


2015 ◽  
Vol 2015 ◽  
pp. 1-9 ◽  
Author(s):  
J. L. Bautista-Jacobo ◽  
E. Rodríguez-Morales ◽  
J. J. Montes-Rodríguez ◽  
H. Gámez-Cuatzín

This work presents a comparative numerical study of the effect of using baffles, and its design, on the behavior of sloshing in a partially filled road tanker carrying LPG. Navier-Stokes equations and standardk-εturbulence model are used to simulate fluid movement; the Volume of Fluid (VOF) method is used to track the liquid-gas interface. Velocity distributions, sloshing stabilization times, and contours of turbulent kinetic energy, which are of high importance in choosing the best design of baffles, are shown. The results show sloshing stabilization times of 22 and 21 s for road tankers with cross-shaped (Type I) and X-shaped (Type II) baffles, respectively, finding lower values of turbulent kinetic energy for Type II design, being, therefore, the best design of baffles for damping of sloshing and vehicle control among studied ones.


Author(s):  
Tobias Barker ◽  
Christophe Prange

AbstractThis paper is concerned with quantitative estimates for the Navier–Stokes equations. First we investigate the relation of quantitative bounds to the behavior of critical norms near a potential singularity with Type I bound $$\Vert u\Vert _{L^{\infty }_{t}L^{3,\infty }_{x}}\le M$$ ‖ u ‖ L t ∞ L x 3 , ∞ ≤ M . Namely, we show that if $$T^*$$ T ∗ is a first blow-up time and $$(0,T^*)$$ ( 0 , T ∗ ) is a singular point then $$\begin{aligned} \Vert u(\cdot ,t)\Vert _{L^{3}(B_{0}(R))}\ge C(M)\log \Big (\frac{1}{T^*-t}\Big ),\,\,\,\,\,\,R=O((T^*-t)^{\frac{1}{2}-}). \end{aligned}$$ ‖ u ( · , t ) ‖ L 3 ( B 0 ( R ) ) ≥ C ( M ) log ( 1 T ∗ - t ) , R = O ( ( T ∗ - t ) 1 2 - ) . We demonstrate that this potential blow-up rate is optimal for a certain class of potential non-zero backward discretely self-similar solutions. Second, we quantify the result of Seregin (Commun Math Phys 312(3):833–845, 2012), which says that if u is a smooth finite-energy solution to the Navier–Stokes equations on $${\mathbb {R}}^3\times (0,1)$$ R 3 × ( 0 , 1 ) with $$\begin{aligned} \sup _{n}\Vert u(\cdot ,t_{(n)})\Vert _{L^{3}({\mathbb {R}}^3)}<\infty \,\,\,\text {and}\,\,\,t_{(n)}\uparrow 1, \end{aligned}$$ sup n ‖ u ( · , t ( n ) ) ‖ L 3 ( R 3 ) < ∞ and t ( n ) ↑ 1 , then u does not blow-up at $$t=1$$ t = 1 . To prove our results we develop a new strategy for proving quantitative bounds for the Navier–Stokes equations. This hinges on local-in-space smoothing results (near the initial time) established by Jia and Šverák (2014), together with quantitative arguments using Carleman inequalities given by Tao (2019). Moreover, the technology developed here enables us in particular to give a quantitative bound for the number of singular points in a Type I blow-up scenario.


2020 ◽  
Vol 14 (4) ◽  
pp. 7369-7378
Author(s):  
Ky-Quang Pham ◽  
Xuan-Truong Le ◽  
Cong-Truong Dinh

Splitter blades located between stator blades in a single-stage axial compressor were proposed and investigated in this work to find their effects on aerodynamic performance and operating stability. Aerodynamic performance of the compressor was evaluated using three-dimensional Reynolds-averaged Navier-Stokes equations using the k-e turbulence model with a scalable wall function. The numerical results for the typical performance parameters without stator splitter blades were validated in comparison with experimental data. The numerical results of a parametric study using four geometric parameters (chord length, coverage angle, height and position) of the stator splitter blades showed that the operational stability of the single-stage axial compressor enhances remarkably using the stator splitter blades. The splitters were effective in suppressing flow separation in the stator domain of the compressor at near-stall condition which affects considerably the aerodynamic performance of the compressor.


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