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Search results for 'large eddy dimulation and related techniques'

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  2. Aircaft Noise - hardcover - VKI LS 2012-02

    Aircaft Noise - hardcover - VKI LS 2012-02

    €170.00

    VKI LS 2012-02 on Aicraft Noise, ISBN-13 978-2-87516-029-4 Learn More
  3. VKI LS 2013-01

    CUBESAT technology and applications - hardcover - VKI LS 2013-01

    €180.00

    CUBESAT technology and applications, ISBN-13 978-2-87516-044-7, VKI LS 2013-01 Learn More
  4. Review of the VKI Doctoral research 2012-2013

    Review of the VKI Doctoral Research 2012-2013 - Free download

    €0.00

    The fourth symposium on the doctoral research of the von Karman Institute for Fluid Dynamics took place during the period March 4 to 6, 2013.

    The articles are downloadable after the checkout.

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  5. Review of the VKI doctoral Research 2010-2011

    Review of the VKI Doctoral Research 2010-2011 - Free download

    €0.00

    The second Symposium on the doctoral research took place at the von Karman Institute for Fluid Dynamics during the period March 1 to 3, 2011. The doctoral students have presented the progress of their research work carried out in the three departments: Aeronautics and Aerospace, Environmental and Applied Fluid Dynamics, Turbomachinery and Propulsion. Learn More
  6. Review of the VKI doctoral Research 2009-2010

    Review of the VKI Doctoral Research 2009-2010 - Free download

    €1.00

    These proceedings aim at giving a snapshot of the research done at the time of the Symposium. Its content is not reviewed by an editorial board and is the property and responsibility of the candidates and their supervisory teams. The idea is to encourage all candidates to write papers on their research even if this research is still under development or if the associated results are only partial. The goal is to train on communication at the best level possible and to offer a yearly compilation of the research accomplished at the Phd level. Learn More
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    Genetic algorithms for optimisation in aeronautics and turbomachinery article pay-per-view 25€/article

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    Genetic algorithms for optimisation in aeronautics and turbomachinery Learn More
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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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    Introduction to optimization methods for multidisciplinary design in aeronautics and turbomachinery article pay-per-view 25€/article

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    Innovative optimization and design techniques, both for aircraft (manned or unmanned UAV/UCAV) and engine systems, are now rapidly moving from research labs to industrial integrated platforms used by collaborative teams. These platforms aim at maximum performance in multidisciplinary context by combining several criteria like aerodynamic efficiency, safety, drag, losses, weight, strength, heat fluxes, emission, noise. To reach concurrently this level of excellence, emergent optimization and design methodologies require more and more robust and efficient associated software for daily use in industrial collaborative design environments.

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    Liquid fragmentation in high-speed flow article pay-per-view 25€/article

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    Liquid injection into compressible crossflow has several interesting applications such as fuel injection in supersonic or hypersonic scramjet engines, thrust vector maneuvering of high speed aerial or space vehicles, and film cooling used in the thermal protection systems of space vehicles that experience atmospheric entry. The field involves many disciplines, and it is a complicated multi-phase flow field especially for compressible crossflow cases, with a unique flow topology including shock-shock and shock-boundary layer interactions. High aerodynamic shear forces, fragmentation, penetration and atomization of the liquid jet are important features that deserve detailed analyses.

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Items 21 to 30 of 48 total

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