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    Implications of Turbine Erosion for an Aero-Engine’s High-Pressure-Turbine Blade’s Low-Cycle-Fatigue Life-Consumption 

    Source: Journal of Engineering for Gas Turbines and Power:;2009:;volume( 131 ):;issue: 005:;page 52501
    Author(s): Muhammad Naeem
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Some in-service deterioration in any mechanical device, such as a military aero-engine, is inevitable. As a result of experiencing any deterioration, an aero-engine will seek a different steady ...
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    Implications of High-Pressure Turbine’s Erosion for a Military Turbofan’s Fuel Consumption 

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 001
    Author(s): Muhammad Naeem
    Publisher: American Society of Civil Engineers
    Abstract: Some in-service deterioration in any mechanical device, such as an aeroengine, is inevitable. As a result of experiencing deterioration (of the engine as a whole or any of its components individually), an engine will seek ...
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    Thermomechanical Response of Profiled Metal-Faced Insulating Sandwich Panels: Testing and Analysis 

    Source: Journal of Structural Engineering:;2024:;Volume ( 150 ):;issue: 006:;page 04024059-1
    Author(s): Muhammad Naeem Tahir; Ehab Hamed
    Publisher: American Society of Civil Engineers
    Abstract: The durability of profiled metal-faced insulating sandwich panels (MFISPs) in terms of exposure to high temperatures and thermal cycles is critical for their use in civil engineering applications. In this paper, a total ...
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