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Search results for 'AERO ENGINE'

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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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    Advanced high-temperature instrumentation for gas turbine applications article pay-per-view 25€/article

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    In aero-engines as well as industrial gas turbines, the drive to higher efficiency is steadily raising the pressures and temperatures in the engines, and this further increases the challenge to instrumentation. Accurate measurements in the hot components of gas turbines (including combustion diagnostics) are recognized as a major need for the assessment of engine component health and performance. High temperature instrumentation is required not only during product development for the validation of new designs or component life prediction methods, but also in service for health monitoring and optimum engine control.

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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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  4. 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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  6. Challenges and applications of active flow control in aero-engines - BACIC, M.

    Challenges and applications of active flow control in aero-engines - BACIC, M.

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    Challenges and applications of active flow control in aero-engines - BACIC, M. – University of Oxford & Rolls-Royce Plc, United Kingdom - https://doi.org/10.35294/ls201704.bacic1

    in Active flow control: techniques and application, Edited by S. Lavagnoli, VKI LS 2017-04, ISBN-13 978-2-87516-116-1, https://doi.org/10.35294/ls201704

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    Industrial compressors article pay-per-view 25€/article

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    VKI LS 1976-91, Industrial compressors, 1976 Learn More
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    Gas turbine engine transient behavior article pay-per-view 25€/article

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    This course presented information and data that are intended to provide an in—depth understanding of gas turbine engine transient behaviour, the modeling methods that are applied to transient events and the simulation technology that supports the transient analysis process. The lecturers represented a cross—section of contributors to the gas turbine engine industry who have specialized in the study of transient engine behaviour.

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    Plasma flow control: Fundamentals, modeling and applications article pay-per-view 25€/article

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    Advances in aero-thermodynamics, aero-elasticity and aero-acoustics largely depend on the understanding of the flow structures, and the ability to control them. The first lecture note reviews the various approaches that are being followed for plasma flow control. The fundamental interaction mechanisms are presented together with the challenges associated to their implementation depending on the flow regime. A presentation on the mechanisms for the generation of momentum transfer using offset dielectric barrier discharges follows, focusing on the physics of the breakdown formation. The next lecture note addresses phenomenological models that can be used in conjunction with CFD codes, from simple algebraic equations to complex set of partial difference equations. The first part is concluded with the use of DBD actuators in various applications for internal and external flow control, over a range of Mach numbers from 0.1 to 3.5, in a wide static pressure range from 0.1 to 9 bar.

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    Advances in aero-acoustics and Thermo-acoustics article pay-per-view 25€/article

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    The accurate modeling of the stability properties of energy transport and conversion processes, such as pipelines, gas turbines, industrial heaters or domestic heating systems, is facing aero-acoustical and thermo-acoustical issues hindering their economic sustainability. The aim of this EU sponsored course notes (Marie-Curie Research Training Network AETHER) is to present the state-of-the-art review in this multi-disciplinary engineering field of aero- and thermo-acoustical coupling in energy conversion processes, in a form accessible to both researchers and industrial engineers.

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