Past

The standard airframe industry tool for flutter analysis is based

on linear potential predictions of the aerodynamics. Despite the

limitations of the modelling this is even true in the transonic

range. There has been a heavy research effort in the past decade to

use CFD to generate the aerodynamics for flutter simulations, to

improve the reliability of predictions and thereby reduce the risk

and cost of flight testing. The first part of the talk will describe

efforts at Glasgow to couple CFD with structural codes to produce

a time domain simulation and an example calculation will be described for

the BAE SYSTEMS Hawk aircraft.

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A drawback with time domain simulations is that unsteady CFD is still

costly and parametric searches to determine stability through the

growth or decay of responses can quickly become impractical. This has

motivated another active research effort in developing ways of

encapsulating the CFD level aerodynamic predictions in models which

are more affordable for routine application. A number of these

approaches are being developed (eg POD, system identification...)

but none have as yet reached maturity. At Glasgow effort has been

put into developing a method based on the behaviour of the

eigenspectrum of the discrete operator Jacobian, using Hopf

Bifurcation conditions to formulate an augmented system of

steady state equations which can be used to calculate flutter speeds

directly. The talk will give the first three dimensional example

of such a calculation.

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For background reports on these topics see

http://www.aero.gla.ac.uk/Research/CFD/projects/aeroelastics/pubs/menu…

We discuss estimating the growth exponents for positive solutions to the

random parabolic Anderson's model with small parameter k. We show that

behaviour for the case where the spatial variable is continuous differs

markedly from that for the discrete case.

The probabilistic approach to homogenization can be adapted to fully

degenerate situations, where irreducibility is insured from a Doeblin type

condition. Using recent results on weak sense Poisson equations in a

similar framework, obtained jointly with A. Veretennikov, together with a

regularization procedure, we prove the homogenization result. A similar

approach can also handle degenerate random homogenization.

It is known for elliptic problems with smooth coefficients

that the solution is smooth in the interior of the domain;

low regularity is only possible near the boundary.

The $hp$-version of the FEM allows us to exploit this

property if we use meshes where the element size grows

porportionally to the element's distance to the boundary

and the approximation order is suitably linked to the

element size. In this way most degrees of freedom are

concentrated near the boundary.

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In this talk, we will discuss convergence and complexity

issues of the boundary concentrated FEM. We will show

that it is comparable to the classical boundary element

method (BEM) in that it leads to the same convergence rate

(error versus degrees of freedom). Additionally, it

generalizes the classical FEM since it does not require

explicit knowledge of the fundamental solution so that

it is also applicable to problems with (smooth) variable

coefficients.