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    Understanding the Effect of Three-Dimensional Design in Tandem Blade 

    Source: Journal of Turbomachinery:;2023:;volume( 146 ):;issue: 003:;page 31002-1
    Author(s): Kumar, Amit; Kumar, Akshay; Chhugani, Hitesh; More, Shubhali; Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In order to maximize the pressure ratio and efficiency, compressor designers have tried several unconventional design approaches. Tandem blading is one such unconventional design that promises a higher pressure ratio per ...
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    Aerodynamics of Sweep in a Tandem-Bladed Subsonic Axial Compressor Rotor 

    Source: Journal of Fluids Engineering:;2022:;volume( 144 ):;issue: 012:;page 121203
    Author(s): Kumar, Amit;John, Jerry T.;Chhugani, Hitesh;Kumar, Akshay;Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The present numerical investigation aims to understand the effect of the chordwise sweep on the performance of a tandem rotor. In a tandem compressor rotor, diffusion is achieved through two smaller airfoils, which are ...
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    Effect of Differential Tip Clearance on the Performance of a Tandem Rotor 

    Source: Journal of Turbomachinery:;2022:;volume( 144 ):;issue: 008:;page 81007-1
    Author(s): Kumar, Amit; Chhugani, Hitesh; More, Shubhali; Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Tandem blade is an interesting concept that promises a higher total pressure rise per stage. Owing to two separate tip leakage vortices and their interaction, losses are likely to increase particularly near the tip region. ...
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