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    Effect of Tip Clearance Dimensions and Control of Unsteady Flows in a Multi-Stage High-Pressure Compressor 

    Source: Journal of Turbomachinery:;2012:;volume( 134 ):;issue: 005:;page 51005
    Author(s): Nicolas Gourdain; Fabien Wlassow; Xavier Ottavy
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the investigations performed to better understand unsteady flows that develop in a three-stage high-pressure compressor. More specifically, this study focuses on rotor-stator ...
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    Analysis of the Interrow Flow Field Within a Transonic Axial Compressor: Part 2—Unsteady Flow Analysis 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 57
    Author(s): Xavier Ottavy; Isabelle Trébinjac; André Vouillarmet
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analysis of the experimental data, obtained by laser two-focus anemometry in the IGV-rotor interrow region of a transonic axial compressor, is presented with the aim of improving the ...
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    Analysis of the Interrow Flow Field Within a Transonic Axial Compressor: Part 1—Experimental Investigation 

    Source: Journal of Turbomachinery:;2001:;volume( 123 ):;issue: 001:;page 49
    Author(s): Xavier Ottavy; Isabelle Trébinjac; André Vouillarmet
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper relates to two-dimensional laser two-focus (L2F) anemometry measurements, conducted in a transonic research high-pressure compressor. Curved glass, which conforms to the shroud contour, ...
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    The Effects of Wake-Passing Unsteadiness Over a Highly Loaded Compressor-Like Flat Plate 

    Source: Journal of Turbomachinery:;2004:;volume( 126 ):;issue: 001:;page 13
    Author(s): Xavier Ottavy; Simon Gallimore; Stephane Vilmin; Howard Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present study is concerned with wake-induced unsteady effects in axial-compressor blade rows. The goal is to exploit these effects in order to design high-lift blades without increasing the ...
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    A High Temperature High Bandwidth Fast Response Total Pressure Probe for Measurements in a Multistage Axial Compressor 

    Source: Journal of Engineering for Gas Turbines and Power:;2012:;volume( 134 ):;issue: 006:;page 61601
    Author(s): Mehmet Mersinligil; Nicolas Courtiade; Xavier Ottavy; Jean-François Brouckaert
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Over the last decades, fast response aerodynamic probes have been recognized as a robust measurement technique to provide time-resolved flow field data in turbomachinery environments. Still, most ...
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