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    Wake Analysis of an Aerodynamically Optimized Boxprop High-Speed Propeller 

    Source: Journal of Turbomachinery:;2019:;volume 141:;issue 009:;page 91011
    Author(s): Patrao, Alexandre Capitao; Grönstedt, Tomas; Lundbladh, Anders; Villar, Gonzalo Montero
    Publisher: American Society of Mechanical Engineers (ASME)
    Abstract: The Boxprop is a novel, double-bladed, tip-joined propeller for high-speed flight. The concept draws inspiration from the box wing concept and could potentially decrease tip vortex strength compared with conventional ...
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    Assessment of CO2 and NOx Emissions in Intercooled Pulsed Detonation Turbofan Engines 

    Source: Journal of Engineering for Gas Turbines and Power:;2019:;volume( 141 ):;issue: 001:;page 11016
    Author(s): Xisto, Carlos; Petit, Olivier; Grönstedt, Tomas; Lundbladh, Anders
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present paper, the synergistic combination of intercooling with pulsed detonation combustion is analyzed concerning its contribution to NOx and CO2 emissions. CO2 is directly proportional to fuel burn and can, ...
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    Generalized Method for the Conceptual Design of Compact Heat Exchangers 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 011:;page 111018-1
    Author(s): Miltén, Petter; Johnsson, Isak; Lundbladh, Anders; Xisto, Carlos
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The paper introduces a novel method for generalized heat exchanger (HX) design and evaluation, freeing the process from predefined geometries. It aims to facilitate early-stage conceptual exploration, allowing the designer ...
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    First and Second Law Analysis of Future Aircraft Engines 

    Source: Journal of Engineering for Gas Turbines and Power:;2014:;volume( 136 ):;issue: 003:;page 31202
    Author(s): Grأ¶nstedt, Tomas; Irannezhad, Mohammad; Lei, Xu; Thulin, Oskar; Lundbladh, Anders
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An optimal baseline turbofan cycle designed for a performance level expected to be available around year 2050 is established. Detailed performance data are given in takeoff, top of climb, and cruise to support the analysis. ...
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