Mediation and the Process of Outer Expansion

2021 ◽  
pp. 21-61
Author(s):  
Camila Mozzini-Alister
Keyword(s):  
AIAA Journal ◽  
1964 ◽  
Vol 2 (8) ◽  
pp. 1511-1512 ◽  
Author(s):  
S. H. LAM ◽  
D. C. LEIGH

1997 ◽  
Vol 07 (05) ◽  
pp. 663-680 ◽  
Author(s):  
Dominique Leguillon

Historically, homogenization of periodic structures has been first investigated by the method of multiple scalings expansions. More recently, an interpretation has been given in terms of averages and effective moduli. Both approaches involve a slow variable at the macroscopic scale, and a fast one at the microscopic level. The periodicity of the solutions with respect to the second variable is a strong assumption made prior to any analysis. Although involving similar calculations, the two approaches differ and it is not so obvious to link them together. The matched asymptotic expansions presented here allow to give a common explanation to the two already mentioned approaches. The first one corresponds to an outer expansion while the second one describes the leading term of an inner expansion. Moreover, no a priori assumption is made, the periodicity of the solutions occurs as a consequence of the structure of the inner problems. The next term (involving a quadratic dependence on the local variable) of the inner expansion can be derived in the same way. The same matched asymptotics process can be used to define homogenized boundary conditions as well as boundary layers. These layers come from a mismatch between the general form of the solution within the domain and the boundary conditions which occur to be a perturbation of the periodicity. Indeed, it is not easy to give an exact definition of the boundary conditions in the original problem, the inner expansion defined on the enlarged domain allows one to give a precise framework for these conditions. They split into two parts, a macroscopic one defined on the smooth (homogenized) boundary and a microscopic periodic fluctuation taking into account the exact shape of the boundary.


1982 ◽  
Vol 119 ◽  
pp. 107-120 ◽  
Author(s):  
K. J. Ruschak

A difficulty in applying the lubrication approximation to flows where a liquid/air interface forms lies in supplying boundary conditions at the point of formation of the interface that are consistent with the lubrication approximation. The method of matched asymptotic expansions is applied to the flow between partially submerged, counter-rotating rollers, a representative problem from this class, and the lubrication approximation is found to generate the first term of an outer expansion of the problem solution. The first term of an inner expansion describes the two-dimensional flow in the vicinity of the interface, and approximate results are found by the finite-element method. Matching between the inner and outer solutions determines boundary conditions on the pressure and the pressure gradient at the point of formation of the interface which allow the solution to the outer, lubrication flow to be completed.


1968 ◽  
Vol 31 (2) ◽  
pp. 379-395 ◽  
Author(s):  
B. W. Thompson

Riegels (1938) investigated the breakdown of Hele-Shaw flow in a Hele-Shaw cell with unusually large separation distance 2h* between the walls. A theoretical outer expansion for the velocity was constructed in the case where the obstacle is a circular cylinder, using an intuitive inner boundary condition that seems to be correct in the limit h* → 0, but without explicit matching with the inner expansion.An inner expansion has now been found, and it shows that the solution in the inner layer forces terms into the outer expansion that are larger than those found by Riegels whenever h* is finite and not zero.


2021 ◽  
Vol 931 ◽  
Author(s):  
Peter A. Monkewitz

The scaling of different features of streamwise normal stress profiles $\langle uu\rangle ^+(y^+)$ in turbulent wall-bounded flows is the subject of a long-running debate. Particular points of contention are the scaling of the ‘inner’ and ‘outer’ peaks of $\langle uu\rangle ^+$ at $y^+\approxeq ~15$ and $y^+ ={O}(10^3)$ , respectively, their infinite Reynolds number limit, and the rate of logarithmic decay in the outer part of the flow. Inspired by the thought-provoking paper of Chen & Sreenivasan (J. Fluid Mech., vol. 908, 2021, p. R3), two terms of an inner asymptotic expansion of $\langle uu\rangle ^+$ in the small parameter $Re_{\tau }^{-1/4}$ are constructed from a set of direct numerical simulations (DNS) of channel flow. This inner expansion is for the first time matched through an overlap layer to an outer expansion, which not only fits the same set of channel DNS within 1.5 % of the peak stress, but also provides a good match of laboratory data in pipes and the near-wall part of boundary layers, up to the highest $Re_{\tau }$ values of $10^5$ . The salient features of the new composite expansion are first, an inner $\langle uu\rangle ^+$ peak, which saturates at 11.3 and decreases as $Re_{\tau }^{-1/4}$ . This inner peak is followed by a short ‘wall log law’ with a slope that becomes positive for $Re_{\tau }$ beyond ${O}(10^4)$ , leading up to an outer peak, followed by the logarithmic overlap layer with a negative slope going continuously to zero for $Re_{\tau }\to \infty$ .


Author(s):  
Gordon E. Andrews ◽  
Nasser T. Ahmad

This work investigates a single axial swirler combustor using flat bladed axial swirlers at atmospheric pressure, 600K preheat, with premixed propane and air. The aim was to investigate the axial swirler design influences on flame stability and NOx emissions, for fully premixed combustion in a single swirler cylindrical combustor configuration. A reference Mach number of 0.05 at 600K was used, which represents all the combustion air passing through the swirler. This maximum swirler airflow is required for the highest turbine entry temperatures with low NOx emissions. The axial swirler design had only a small influence on the weak extinction, but it had a greater influence on NOx. The swirlers with a large central hub had greater NOx emissions, as this created a larger central recirculation zone and greater residence time of the hottest part of the flame. It was preferable to stabilise the flame with an outer expansion shear layer as this minimised the size of the inner recirculation zone and this minimised the NOx. The influence of the swirl angle, 30, 45 or 60° for the same flow capacity was that the swirler had to be a larger diameter as the vane angle was increased, to keep the blockage and pressure loss the same. This removed the possibility of having either an inner or outer flow expansion for the 60° swirler, but the flow expansions were maximised for the 30° swirler. The effect of the swirl vane angle on NOx was mainly due to the associated changes in the flow expansion. 45° swirlers with no central hub and a large outer expansion were the best design for the lowest NOx emissions and could achieve 15ppm NOx at 15% oxygen at 2000K.


2005 ◽  
Vol 73 (2) ◽  
pp. 183-188
Author(s):  
J. G. Simmonds

An acceptable variant of the Koiter–Morley equations for an elastically isotropic circular cylindrical shell is replaced by a constant coefficient fourth-order partial differential equation for a complex-valued displacement-stress function. An approximate formal solution for the associated “free-space” Green’s function (i.e., the Green’s function for a closed, infinite shell) is derived using an inner and outer expansion. The point wise error in this solution is shown rigorously to be of relative order (h∕a)(1+h∕a∣x∣), where h is the constant thickness of the shell, a is the radius of the mid surface, and ax is distance along a generator of the mid surface.


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