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    Effect of system rotation on turbulence with applications to turbomachinery 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 extemal 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. The second part of the proceedings starts with the analysis of the goveming equations of glow discharges in supersonic and hypersonic flows. The estimations of characteristics time scales in high speed flow highlight the influence of gas motion on the electro-dynamic structure. The second course note demonstrates successful plasma applications in the lab at high speed, for drag reduction, plasma-induced generation of shock waves, and artificial flow separation. The third lecture note describes recent experimental and computational research in identifying and modeling the gasdynamic and therrnochemical processes of the plasmoid generation with micro—wave and laser discharge.

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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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  3. wind tunnel qualification, heat-flux measurement, adiabatic-wall temperature measurement, unsteady temperature, unsteady pressure, supersonic boundary layer, roughnessinduced transition, shock-wave/boundary-layer interaction

    Experimental investigation of induced supersonic boundary layer transition

    €25.00

    VKI PHDT 2014-07, Henny Bottini, Experimental investigation of induced supersonic boundary layer transition, ISBN 978-2-87516-069-0, 184 pgs Learn More
  4. Experimental aerothermal performance of turbofan bypass flow heat exchangers

    Experimental aerothermal performance of turbofan bypass flow heat exchangers

    €25.00

    VKI PHDT 2014-06, Laura Roca Villafañe, Experimental aerothermal performance of turbofan bypass flow heat exchangers, ISBN 978-2-87516-070-6, 160 pgs Learn More
  5. 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
  6. Ground Testing Investigation of Hypersonic Transition Phenomena for a Re-entry Vehicle

    Ground Testing Investigation of Hypersonic Transition Phenomena for a Re-entry Vehicle

    €25.00

    VKI PHDT 2013-11, Davide Masutti, Ground Testing Investigation of Hypersonic Transition Phenomena for a Re-entry Vehicle, IISBN 978-2-87516-052-2, 170 pgs Learn More
  7. Review of the VKI doctoral Research 2010-2011

    Review of the VKI Doctoral Research 2010-2011 - Free download

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    The second Symposium on the doctoral research took place at the von Karman Institute for Fluid Dynamics during the period March 1 to 3, 2011. The doctoral students have presented the progress of their research work carried out in the three departments: Aeronautics and Aerospace, Environmental and Applied Fluid Dynamics, Turbomachinery and Propulsion. Learn More
  8. 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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