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Product search results for 'gas turbine applications'

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  2. Advanced measurement techniques for aero engines and stationary

    Advanced measurement techniques for aero engines and stationary gas turbines

    €120.00

    VKI LS 2004-04, Advanced measurement techniques for aero engines and stationary gas turbines, ISBN 2-930389-53-2 Learn More
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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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    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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  6. Small high pressure ratio turbines - article pay-per-view - 25€ / article

    Small high pressure ratio turbines - article pay-per-view - 25€ / article

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    Applications for this type of turbines range from small gas turbine engines for light helicopters through airborne and land-based auxiliary power units, automotive powerplants, turboexpanders, mechanical drive steam turbines, solar powerplants working with organic fluids and turbopumps for liquid fuel rockets. Depending on the application, the turbines may be of the radial, axial or mixed flow type. The combination of small blade heights and high Mach numbers and turning angles makes the design of these turbines particularly arduous, especially if the rotor inlet Mach numbers are supersonic. Extensive design experience and the use of advanced design tools can overcome these problems as was demonstrated by the group of lecturers who were selected for this course. The lectures addressed primarily turbine design and development engineers. But testing techniques and advanced calculation methods were also discussed. 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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