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Product search results for 'aero engine design'

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    Aero-Engine design: From state-of-the-art Turbofans article pay-per-view 25€/article

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    The first lectures notes focus on the preliminary design of state of the art turbofan engine for the propulsion of civil aircraft. Issues like thermodynamic cycle, mission analysis, and off design operation (operating line) are addressed. Practical examples are presented. Once this important phase is completed, the different design teams have the boundary conditions to start the design of each component.

    VKI LS 2008-03

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    Combustion in aero engines article pay-per-view 25€/article

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    High pressure two-phase air-kerosene reacting flow, with high levels of turbulence and heat transfer submitted to acoustic waves: this is how the flow in an aero engine combustor could be characterized

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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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    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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    Introduction to optimization and multidisciplinary design in aeronautics and turbomachinery article pay-per-view 25€/article

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    Innovative optimization and design techniques for modern aircraft (manned or UAV/UCAV) and engine systems aiming at maximum performance in a multidisciplinary context (aerodynamic efficiency, safety, drag, losses, weight, strength, heat fluxes, emission, noise, …), are now rapidly moving from research labs to industrial real and virtual platforms. To reach concurrently this level of excellence, emergent optimization methodologies require more and more robust and efficient associated software for a daily use in industrial collaborative design environments.

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  10. Review of the VKI doctoral Research 2011-2012

    Review of the VKI Doctoral Research 2011-2012 - Free download

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    The third Symposium on the doctoral research took place at of the von Karman Institute for Fluid Dynamics took place during the period March 5 to 7, 2012. The doctoral students have presented the progress of their research work carried out in the 3 departments. Learn More

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