dc.contributor.author | Verstraete, T | en_US |
dc.contributor.author | Müller, L | en_US |
dc.contributor.author | Müller, JD | en_US |
dc.contributor.author | EuroTurbo | en_US |
dc.date.accessioned | 2018-10-23T09:50:06Z | |
dc.date.available | 2017-03-11 | en_US |
dc.date.issued | 2017-04-01 | en_US |
dc.date.submitted | 2018-10-17T17:50:53.028Z | |
dc.identifier.issn | 2410-4833 | en_US |
dc.identifier.uri | http://qmro.qmul.ac.uk/xmlui/handle/123456789/47864 | |
dc.description.abstract | Copyright © by the Authors. The aim of this paper is to reduce the pressure losses of a U-bend passage of a turbine blade serpentine cooling channel. A steady state Reynolds-Averaged density based Navier-Stokes solver is used to predict the pressure losses at a Reynolds number of 40,000. A novel geometry representation approach is used defining directly the volume of the passage rather than its exterior boundary, which is now the most common approach in CAD systems. The U-bend volume is parameterised using tri-variate B-splines, the deformations of the shape are controlled by the external control points of the B-spline volume, while the internal control points are repositioned using a transfinite interpolation to ensure a smooth and regular internal representation of the shape. This approach ensures a good grid regularity at a large reduced computational cost compared to traditional approaches. The sensitivities of the control points with respect to the objective function are computed using a hand-derived adjoint solver and geometry generation system. A one-shot approach is used to simultaneously converge flow, gradient and design, resulting in a rapid design approach with a design time equivalent to approximately 10 normal CFD runs. A large reduction in pressure loss is obtained, and the optimal geometry is analysed in more detail. | en_US |
dc.rights | This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY-NC-ND) license ( https://creativecommons.org/licenses/by-nc-nd/4.0/). | |
dc.title | Adjoint based design optimisation of an internal cooling channel u-bend for minimized pressure losses | en_US |
dc.type | Conference Proceeding | |
dc.rights.holder | © 2017 by the authors. Licensee MDPI, Basel, Switzerland. | |
pubs.notes | Not known | en_US |
pubs.publication-status | Published | en_US |
dcterms.dateAccepted | 2017-03-11 | en_US |