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    Unsteady Aerodynamic Forcing Due to Distortion in a Boundary Layer Ingesting Fan 

    Source: Journal of Turbomachinery:;2024:;volume( 146 ):;issue: 007:;page 71008-1
    Author(s): Mårtensson, Hans; Billson, Mattias
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Boundary Layer Ingestion (BLI) is a concept with the potential to reduce energy consumption needed for aircraft propulsion. For the fan this results in a need to work well in an environment of increased continuous distortion. ...
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    Aeroacoustic Effects on the Forcing of Fan and Compressor Blades Due to Distortion 

    Source: Journal of Engineering for Gas Turbines and Power:;2024:;volume( 146 ):;issue: 006:;page 61013-1
    Author(s): Mårtensson, Hans; Billson, Mattias
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A distorted air stream entering an aeroengine fan or compressor leads to harmonic forces on the rotating blades. These aerodynamically induced forces are well-known causes of blade vibration and associated fatigue problems. ...
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    The Impact of Manufacturing Variations on Performance of a Transonic Axial Compressor Rotor 

    Source: Journal of Turbomachinery:;2020:;volume( 142 ):;issue: 008:;page 081009-1
    Author(s): Lejon, Marcus; Andersson, Niklas; Ellbrant, Lars; Mårtensson, Hans
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, the impact of manufacturing variations on performance of an axial compressor rotor is evaluated at design rotational speed. The geometric variations from the design intent obtained from measurements were ...
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    Forced Response Analysis of a Mistuned, Compressor Blisk Comparing Three Different Reduced Order Model Approaches 

    Source: Journal of Engineering for Gas Turbines and Power:;2017:;volume( 139 ):;issue: 006:;page 62501
    Author(s): Salas, Mauricio Gutierrez; Bladh, Ronnie; Mårtensson, Hans; Petrie-Repar, Paul; Fransson, Torsten; Vogt, Damian M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Accurate structural modeling of blisk mistuning is critical for the analysis of forced response in turbomachinery. Apart from intentional mistuning, mistuning can be due to the manufacturing tolerances, corrosion, foreign ...
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