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    Closure to “Discussion of ‘Measurement of the Three-Dimensional Tip Region Flow Field in an Axial Compressor’” (1993, ASME J. Turbomach., 115, p. 476) 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 476
    Author(s): R. C. Stauter
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Measurement of the Three-Dimensional Tip Region Flow Field in an Axial Compressor 

    Source: Journal of Turbomachinery:;1993:;volume( 115 ):;issue: 003:;page 468
    Author(s): R. C. Stauter
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A two-color, five-beam LDV system has been configured to make simultaneous three-component velocity measurements of the flow field in a two-stage axial compressor model. The system has been used ...
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    Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part 1—Experiment 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 219
    Author(s): R. C. Stauter; R. P. Dring; F. O. Carta
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The fluid dynamics of turbomachines are extremely complex, due in part to the aerodynamic interactions between rotors and stators. It is necessary to acquire fluid dynamic data that reflect the ...
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    Closure to “Discussion of ‘Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part 1—Experiment’” (1991, ASME J. Turbomach., 113, p. 226) 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 226
    Author(s): R. C. Stauter; R. P. Dring; F. O. Carta
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Temporally and Spatially Resolved Flow in a Two-Stage Axial Compressor: Part 2—Computational Assessment 

    Source: Journal of Turbomachinery:;1991:;volume( 113 ):;issue: 002:;page 227
    Author(s): K. L. Gundy-Burlet; R. C. Stauter; R. P. Dring; M. M. Rai
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Fluid dynamics of turbomachines are complicated because of aerodynamic interactions between rotors and stators. It is necessary to understand the aerodynamics associated with these interactions in ...
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