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Product search results for 'AERO ENGINE'

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  1. Article pay-per-view

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

    €0.00

    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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  2. Combustion in aero engines

    Combustion in aero engines - hardcover

    €160.00

    VKI LS 2010-03, Combustion in aero engines, hardcover, 1 volume, ISBN 978-2-87516-001-0 Learn More
  3. Combustion in aero-engines - hardcover

    Combustion in aero-engines - hardcover

    €180.00

    Combustion in aero-engines, VKI LS 2012-04, ISBN-13 978-2-87516-036-2 Learn More
  4. 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
  5. VKI LS 2013-04

    Aeroengine design: from state of the art of turbofans towards innovative architectures - hardcover

    €190.00

    Aeroengine design: from state of the art of turbofans towards innovative architectures, VKI LS 2013-04, ISBN-13 978-2-87516-050-8 Learn More
  6. Article pay-per-view

    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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    Aero-engine design: A state of the art article pay-per-view 25€/article

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    Aero-engine design: A state of the art article pay-per-view 25€/article Learn More
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  9. 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
  10. Aero-thermal impact of purge flow and rotor platform

    Aero-thermal impact of purge flow and rotor platform film cooling on a transonic HP turbine stag

    €25.00

    VKI PHDT 2009-08, Marco Pau, Aero-thermal impact of purge flow and rotor platform film cooling on a transonic HP turbine stage, ISBN 978-2-930389-41-9, 138 pgs Learn More

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