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    Discussion: “Loss Sources and Magnitudes in Axial-Flow Compressors” (Koch, C. C., and Smith, Jr., L. H., 1976, ASME J. Eng. Power, 98, pp. 411–424) 

    Source: Journal of Engineering for Gas Turbines and Power:;1977:;volume( 099 ):;issue: 002:;page 297
    Author(s): N. L. Sanger
    Publisher: The American Society of Mechanical Engineers (ASME)
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    The Use of Optimization Techniques to Design-Controlled Diffusion Compressor Blading 

    Source: Journal of Engineering for Gas Turbines and Power:;1983:;volume( 105 ):;issue: 002:;page 256
    Author(s): N. L. Sanger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A method is presented for automating compressor blade design using numerical optimization and is applied to the design of a controlled diffusion stator blade row. A general purpose optimization ...
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    An Experimental Investigation of Several Low-Area-Ratio Water Jet Pumps 

    Source: Journal of Fluids Engineering:;1970:;volume( 092 ):;issue: 001:;page 11
    Author(s): N. L. Sanger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Several low-area-ratio jet pumps were evaluated experimentally in water. Principal geometrical variables investigated were area ratio, throat length, and nozzle spacing. Diffuser geometry was also ...
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    Design of a Low Aspect Ratio Transonic Compressor Stage Using CFD Techniques 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 003:;page 479
    Author(s): N. L. Sanger
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A transonic compressor stage has been designed for the Naval Postgraduate School Turbopropulsion Laboratory. The design relied heavily on CFD techniques while minimizing conventional empirical ...
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    Comparison of Calculated and Experimental Cascade Performance for Controlled-Diffusion Compressor Stator Blading 

    Source: Journal of Turbomachinery:;1986:;volume( 108 ):;issue: 001:;page 42
    Author(s): N. L. Sanger; R. P. Shreeve
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The midspan section of a previously reported controlled-diffusion compressor stator has been experimentally evaluated in cascade. Measurements were taken over a range of incidence angles for blade ...
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    Design and Performance of a Fixed, Nonaccelerating Guide Vane Cascade That Operates Over an Inlet Flow Angle Range of 60 Deg 

    Source: Journal of Engineering for Gas Turbines and Power:;1985:;volume( 107 ):;issue: 002:;page 477
    Author(s): J. M. Sanz; E. R. McFarland; N. L. Sanger; T. F. Gelder; R. H. Cavicchi
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A unique set of wind tunnel guide vanes are designed with an inverse design code and analyzed with a panel method and an integral boundary layer code developed at the NASA Lewis Research ...
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