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    Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 010:;page 101007-1
    Author(s): Raduev, Zelimhan; Jackson, Dougal; Chowdhury, Nafiz; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we consider the impact of trailing edge burn-back on the aerodynamic performance of cooled transonic high-pressure nozzle guide vanes. We consider four levels of burn-back ranging from new parts to severely ...
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    Impact of Nozzle Guide Vane Trailing Edge Damage on High-Pressure Turbine Stage Performance 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:008:;page 115
    Author(s): Raduev, Zelimhan; Jackson, Dougal; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In this paper we consider the impact of nozzle guide vane trailing edge burn-back (damage) on cooled high-pressure turbine stage performance. We analyse four levels of simulated burn-back ranging from new parts ...
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    Impact of Trailing Edge Damage on Nozzle Guide Vane Flow Capacity 

    Source: Journal of Turbomachinery:;2026:;volume( 148 ):;issue:003
    Author(s): Raduev, Zelimhan; Jackson, Dougal; Chowdhury, Nafiz; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. In this paper, we consider the impact of trailing edge burn-back (due to oxidation damage) on the flow capacity of cooled transonic high-pressure (HP) nozzle guide vanes. The purpose is to provide understanding ...
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    Impact of Trailing Edge Damage on Nozzle Guide Vane Aerodynamic Performance 

    Source: Journal of Turbomachinery:;2025:;volume( 147 ):;issue: 010:;page 101007-1
    Author(s): Raduev, Zelimhan; Jackson, Dougal; Chowdhury, Nafiz; Povey, Thomas
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In this paper, we consider the impact of trailing edge burn-back on the aerodynamic performance of cooled transonic high-pressure nozzle guide vanes. We consider four levels of burn-back ranging from new parts to severely ...
    Request PDF
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
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