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    Rotating Probe Measurements of the Pump Passage Flow Field in an Automotive Torque Converter 

    Source: Journal of Fluids Engineering:;2001:;volume( 123 ):;issue: 001:;page 81
    Author(s): Y. Dong; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The relative flow in an automotive torque converter pump passage was measured at three locations inside the passage (mid-chord, 3/4-chord, and 4/4-chord) using a miniature high-frequency response ...
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    Experimental Investigation of the Flow Field in an Automotive Torque Converter Stator 

    Source: Journal of Fluids Engineering:;1999:;volume( 121 ):;issue: 004:;page 788
    Author(s): Y. Dong; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The flow field at the exit of a torque converter stator exit was measured using a miniature conventional five-hole probe. The data at speed ratio 0.8, 0.6, and 0.065 are presented. At the ...
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    Compressor Blade Boundary Layers: Part 1—Test Facility and Measurements With No Incident Wakes 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 222
    Author(s): Y. Dong; N. A. Cumpsty
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The boundary layers on compressor blades are sensitive to the conditions at which transition occurs and transition can be affected by the convection of wakes from upstream blade rows. This ...
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    Compressor Blade Boundary Layers: Part 2—Measurements With Incident Wakes 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 231
    Author(s): Y. Dong; N. A. Cumpsty
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper follows directly from Part 1 by the same authors and describes measurements of the boundary layer on a supercritical-type compressor blade with wakes from a simulated moving upstream ...
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    Discussion: “The Measurement of Boundary Layers on a Compressor Blade in Cascade: Part 4—Flow Fields for Incidence Angles of −1.5 and −8.5 Degrees” (Zierke, W. C., and Deutsch, S., 1990, ASME J. Turbomach., 112, pp. 241–255) 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 255
    Author(s): N. A. Cumpsty; Y. Dong
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Three-Dimensional Separated Flow Field in the Endwall Region of an Annular Compressor Cascade in the Presence of Rotor-Stator Interaction: Part 2—Unsteady Flow and Pressure Field” (Schulz, H. D., Gallus, H. E., and Lakshminarayana, B., 1990, ASME J. Turbomach., 112, pp. 679–688) 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 004:;page 688
    Author(s): N. A. Cumpsty; Y. Dong
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Discussion: “Viscous Flow in a Controlled Diffusion Compressor Cascade With Increasing Incidence” (Elazar, Y., and Shreeve, R. P., 1990, ASME J. Turbomach., 112, pp. 256–265) 

    Source: Journal of Turbomachinery:;1990:;volume( 112 ):;issue: 002:;page 266
    Author(s): N. A. Cumpsty; Y. Dong
    Publisher: The American Society of Mechanical Engineers (ASME)
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    Experimental and Numerical Investigation of Stator Exit Flow Field of an Automotive Torque Converter 

    Source: Journal of Turbomachinery:;1996:;volume( 118 ):;issue: 004:;page 835
    Author(s): B. V. Marathe; B. Lakshminarayana; Y. Dong
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The objective of this investigation is to understand the nature of the complex flow field inside each element of the torque converter through a systematic experimental and numerical investigation ...
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    Steady and Unsteady Flow Field at Pump and Turbine Exits of a Torque Converter 

    Source: Journal of Fluids Engineering:;1998:;volume( 120 ):;issue: 003:;page 538
    Author(s): Y. Dong; D. Maddock; B. Lakshminarayana
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The steady and unsteady flow field at the pump and the turbine exit of a 245 mm diameter automotive torque converter was measured by a miniature high-frequency-response five-hole probe and a ...
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    Three-Dimensional Flows and Loss Reduction in Axial Compressors 

    Source: Journal of Turbomachinery:;1987:;volume( 109 ):;issue: 003:;page 354
    Author(s): Y. Dong; S. J. Gallimore; H. P. Hodson
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Measurements have been performed in a low-speed high-reaction single-stage axial compressor. Data obtained within and downstream of the rotor, when correlated with the results of other investigations, ...
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