Welcome to the von Karman Institute for Fluid Dynamics Store

Product search results for 'combustion in aero engines'

Items 1 to 10 of 128 total

per page
Page:
  1. 1
  2. 2
  3. 3
  4. 4
  5. 5

Grid  List 

Set Ascending Direction
  1. 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
  2. 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

    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. Article pay-per-view

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

    €0.00

    Aero-engine design: A state of the art article pay-per-view 25€/article Learn More
  5. Article pay-per-view

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

    €0.00

    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

    Learn More
  6. 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
  7. Article pay-per-view

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

    €0.00

    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.

    Learn More
  8. Article pay-per-view

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

    €0.00

    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.

    Learn More
  9. On the Aerothermal Flow Field in a Transonic HP Turbine Stage with a Multi-Profile LP Stator Vane

    On the Aerothermal Flow Field in a Transonic HP Turbine Stage with a Multi-Profile LP Stator Vane

    €25.00

    VKI PHDT 2013-09, Sergio Lavagnoli, On the Aerothermal Flow Field in a Transonic HP Turbine Stage with a Multi-Profile LP Stator Vane, ISBN 978-2-87516-042-3, 165 pgs Learn More
  10. 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

Items 1 to 10 of 128 total

per page
Page:
  1. 1
  2. 2
  3. 3
  4. 4
  5. 5

Grid  List 

Set Ascending Direction