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    Transonic Flow Around Rotor Blade Elements 

    Source: Journal of Fluids Engineering:;1975:;volume( 097 ):;issue: 004:;page 598
    Author(s): J. W. Kurzrock; A. S. Novick
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: An analytical/numerical method for calculating blade-to-blade transonic flow fields around blade elements of an axial compressor rotor of a turbomachine is presented. Radius variation and stream ...
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    Design and Preliminary Results of a Fuel Flexible Industrial Gas Turbine Combustor 

    Source: Journal of Engineering for Gas Turbines and Power:;1982:;volume( 104 ):;issue: 002:;page 368
    Author(s): A. S. Novick; H. G. Yacobucci; D. L. Troth
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The work described in this paper is a part of the DOE/LeRc “Advanced Conversion Technology Project” (ACT). The program is a multiple contract effort with funding provided by the Department of ...
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    An Experimental Determination of the Unsteady Aerodynamics in a Controlled Oscillating Cascade 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 001:;page 88
    Author(s): S. Fleeter; A. S. Novick; R. E. Riffel; J. E. Caruthers
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A unique supersonic inlet flow field unsteady cascade experiment is described wherein the time-dependent pressure distribution within an harmonically oscillating airfoil cascade is quantitatively ...
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