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    Response of a Tandem-Staged Compressor to Circumferential Inflow Distortion 

    Source: Journal of Fluids Engineering:;2022:;volume( 144 ):;issue: 009:;page 91202-1
    Author(s): Kumar, Amit; Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Tandem rotor, as a concept, promises a higher diffusion capacity than a single rotor. However, it is reported to have a lower operating range than the conventional rotor. Inflow distortion can lead to significant changes ...
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    Influence of Circumferential Inflow Distortion on the Performance of a Low Speed, High Aspect Ratio Contra Rotating Axial Fan 

    Source: Journal of Turbomachinery:;2014:;volume( 136 ):;issue: 007:;page 71009
    Author(s): Mistry, Chetan; Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The influence of circumferential inflow distorted on the performance and flow behavior of a high aspect ratio, low speed contra rotating fan is reported in this paper. The total pressure at the inlet is artificially distorted ...
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    Benefits of Nonaxisymmetric Endwall Contouring in a Compressor Cascade With a Tip Clearance 

    Source: Journal of Fluids Engineering:;2015:;volume( 137 ):;issue: 005:;page 51101
    Author(s): Varpe, Mahesh K.; Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the design of a nonaxisymmetric hub contouring in a shroudless axial flow compressor cascade operating at near stall condition. Although an optimum tip clearance (TC) reduces the total pressure loss, ...
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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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    Windmilling Characteristics of a Contra-Rotating Fan 

    Source: Journal of Engineering for Gas Turbines and Power:;2021:;volume( 143 ):;issue: 008:;page 081004-1
    Author(s): Manas, M. P.; Karmakar, Arghya; Pradeep, A. M.
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: In the present experimental study, a low aspect ratio, low hub-tip ratio contra-rotating axial fan is investigated to understand its performance under windmilling conditions. Two configurations are tested; in the first ...
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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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