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Search results for 'Wind turbine aerodynamics : a state-of-the-art'

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    Internal cooling in turbomachinary article pay-per-view 25€/article

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    The aim of these Lecture Series proceedings is to look at the state of the art achievements in internal cooling systems, both from an experimental as from a computational point of view. Although most of the lecturers come from the turbomachinery community, this Lecture Series notes are also of interest for those interested in various forced convection heat transfer and cooling problems.

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    Turbulent combustion article pay-per-view 25€/article

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    The objective of these Lecture Series proceedings on Turbulent Combustion is to present the state-of-the-art review of on-going activities in turbulent combustion and to outline current research directions. Introductory lecture notes on the fundamentals of combustion, and in particular of turbulent combustion, are followed by up-to-date reviews on numerical modeling and experimental results in single and two-phase flows.

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    Particle image velocimetry: general introduction to the technique article pay-per-view 25€/article

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    Particle Image Velocimetry (PIV) has appeared 25 years ago and since the beginning it has drastically improved in all fields. At the same time this technique becomes became more and more utilized in fluid dynamic laboratories from research institutes and industry and it is used now in a very large range of applications. After its first appearance in the laboratories, the PIV technique has benefited of the progress in the LASER technologies as well as electronic image recording, which considerably enhanced its potential. PIV has also taken advantage of several developments made in the processing algorithms in these two decades. This spectacular evolution has been largely supported through European collaborative projects such as EuroPIV and PivNet.

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    35Th CFD/ADIGMA course on very high order discretization methods article pay-per-view 25€/article

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    Schemes with order of accuracy higher than two have become an important subject of research in CFD, and the perspective of applying them in industrial aeronautical context is realistic within the next decade. In these course notes the basics and state of the art of the following methods are discussed in detail: Discontinuous Galerkin Finite Element methods; Spectral Element and Spectral Finite Volume methods; Residual Distribution methods. An effort was made to introduce the methods on model problems before applying them to the compressible and incompressible Navier-Stokes equations. Basic ideas like convergence analysis, a priori and duality based error estimates or adjoint consistency and shock capturing are discussed in much detail. Implementation issues are treated, such as efficient quadrature, parallelization, memory consumption and treatment of curved walls. Applications targeted are mainly in the area of steady and unsteady compressible aerodynamics, including transonic and supersonic flow.

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    Structural design of aircraft engines: Key obectives and techniques article pay-per-view 25€/article

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    The continuous trend in weight reduction together with novel engine architectures results in large structural and thermal loads, with narrower security margins. The lecture note on aircraft engine reviews the main challenges of structural design of an aircraft engine, and the associated certification constraints. The first part of these proceedings addresses the engine behaviour (whole engine dynamics, impacts, and thermal loads). Whole Engine dynamics overviews how to model the different elements of the engine to study the dynamic behaviour of the assembled system while respecting design criteria. Foreign object damage and fan blade out describes the methodologies currently used to perform simulations in compressor blades to predict the integrity of the structure.

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    Experimental determination of dynamic stability parameters article pay-per-view 25€/article

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    The stability of aerial vehicles has always been one of the most important topics studied for a safe and smooth flight. An aerial vehicle should have the tendency to return back to a stable position, when it is disturbed from its original path. Dynamic stability is usually thought as the vehicle's response over time when disturbed from a given angle of attack, slip or bank. The advent of flight at high angles of attack has revived our interest in the dynamic stability of aircrafts and missiles. One of the biggest problems in studying dynamic stability is the accurate determination of dynamic stability parameters, in other words, the damping coefficients.

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  7. Turbulent Combustion VKIS LS 2015-03

    Turbulent combustion - hardcover VKI LS 2015-03

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    Turbulent combustion, VKI LS 2015-03, ISBN-13 978-2-87516-087-4 Learn More
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    Film cooling science and technology for gas turbines: State-of-the-art experimental and computational knowledge article pay-per-view 25€/article

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    Film cooling science and technology for gas turbines: State-of-the-art experimental and computational knowledge Learn More
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Items 21 to 30 of 469 total

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