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    Predictions of Endwall Losses and Secondary Flows in Axial Flow Turbine Cascades 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 002:;page 229
    Author(s): O. P. Sharma; T. L. Butler
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the development of a semi-empirical model for estimating end-wall losses. The model has been developed from improved understanding of complex endwall secondary flows, acquired ...
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    Evaluation of Flow Field Approximations for Transonic Compressor Stages 

    Source: Journal of Turbomachinery:;1997:;volume( 119 ):;issue: 003:;page 445
    Author(s): D. J. Dorney; O. P. Sharma
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow through gas turbine compressors is often characterized by unsteady, transonic, and viscous phenomena. Accurately predicting the behavior of these complex multi-blade-row flows with unsteady ...
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    Influence of Endwall Flow on Airfoil Suction Surface Midheight Boundary Layer Development in a Turbine Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 001:;page 147
    Author(s): O. P. Sharma; R. A. Graziani
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents the results of an analysis to assess the influence of cascade passage endwall flow on the airfoil suction surface midheight boundary layer development in a turbine cascade. ...
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    Performance Improvement Through Indexing of Turbine Airfoils: Part 2—Numerical Simulation 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 636
    Author(s): L. W. Griffin; F. W. Huber; O. P. Sharma
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An experimental/analytical study has been conducted to determine the performance improvements achievable by circumferentially indexing succeeding rows of turbine stator airfoils. A series of tests ...
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    Assessment of Unsteady Flows in Turbines 

    Source: Journal of Turbomachinery:;1992:;volume( 114 ):;issue: 001:;page 79
    Author(s): O. P. Sharma; G. F. Pickett; R. H. Ni
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The impacts of unsteady flow research activities on flow simulation methods used in the turbine design process are assessed. Results from experimental investigations that identify the impact of ...
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    Unsteady Three-Dimensional Turbine Aerodynamics 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002:;page 322
    Author(s): H. D. Joslyn; O. P. Sharma; R. P. Dring
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: High response aerodynamic measurements were made in a large-scale, axial, flow turbine model to study the unsteadiness and three dimensionality of the flow. High response velocity vector and ...
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    Boundary Layer Development on Turbine Airfoil Suction Surfaces 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 003:;page 698
    Author(s): O. P. Sharma; R. H. Schlinker; D. A. Bailey; R. A. Wells
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents results of a study, supported by NASA Contract NAS3-20646 under the Energy Efficient Engine Program, conducted to investigate the development of boundary layers under the ...
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    Integrated Control of Rotating Stall and Surge in High-Speed Multistage Compression Systems 

    Source: Journal of Turbomachinery:;1998:;volume( 120 ):;issue: 003:;page 440
    Author(s): K. M. Eveker; D. L. Gysling; C. N. Nett; O. P. Sharma
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Aeroengines operate in regimes for which both rotating stall and surge impose low-flow operability limits. Thus, active control strategies designed to enhance operability of aeroengines must address ...
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    Performance Improvement Through Indexing of Turbine Airfoils: Part 1—Experimental Investigation 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 630
    Author(s): F. W. Huber; O. P. Sharma; S. W. Gaddis; J. B. Staubach; P. D. Johnson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the results of a study to determine the performance improvements achievable by circumferentially indexing successive rows of turbine stator airfoils. An experimental/analytical ...
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    Influence of Compressor Deterioration on Engine Dynamic Behavior and Transient Stall-Margin 

    Source: Journal of Turbomachinery:;2000:;volume( 122 ):;issue: 003:;page 477
    Author(s): Z. S. Spakovszky; J. B. Gertz; J. D. Paduano; A. H. Epstein; O. P. Sharma; E. M. Greitzer
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents an experimental and analytical investigation of compressor stability assessment during engine transient operation. A two-dimensional, linear, compressible, state-space analysis of ...
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