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Product search results for 'Wind turbine aerodynamics: A state-of-the-art. ed. / J.-F. Brouckaert. Rhode Saint Genese : von Karman Institute for Fluid Dynam'

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  2. Aero-thermal performance of a film-cooled high pressure turbine blade/vane: a test case for numerical codes validation

    Aero-thermal performance of a film-cooled high pressure turbine blade/vane: a test case for numerical codes validation

    €25.00

    VKI PHDT 2014-09, Fabrizio Fontaneto, Aero-thermal performance of a film-cooled high pressure turbine blade/vane: a test case for numerical codes validation, ISBN 978-2-87516-083-6, 167 pgs 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
  4. Verification and validation of computational fluid dynamics

    Verification and validation of computational fluid dynamics - hardcover

    €60.00

    VKI LS 2000-08, Verification and validation of computational fluid dynamics Learn More
  5. 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
  6. Advanced measuring techniques for supersonic flows

    Advanced measuring techniques for supersonic flows

    €120.00

    VKI LS 2005-01, Advanced measuring techniques for supersonic flows, ISBN 2-930389-57-5 Learn More
  7. Unsteady aerodynamic stator-rotor interaction in high pressure t

    Unsteady aerodynamic stator-rotor interaction in high pressure turbines

    €25.00

    VKI PHDT 2006-08, Unsteady aerodynamic stator-rotor interaction in high pressure turbines, ISBN 978-2-930389-26-5 Learn More
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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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    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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