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    Activation of Nanoflows for Fuel Cells 

    Source: Journal of Nanotechnology in Engineering and Medicine:;2012:;volume( 003 ):;issue: 002:;page 25201
    Author(s): Z. Insepov; R. J. Miller
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Propagation of Rayleigh traveling waves from a gas on a nanotube surface activates a macroscopic flow of the gas (or gases) that depends critically on the atomic mass of the gas. Our molecular ...
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    Generation of Submicrometer Particles in Dry Sliding Contact 

    Source: Journal of Tribology:;1990:;volume( 112 ):;issue: 004:;page 684
    Author(s): J. L. Xuan; R. J. Miller; H. S. Cheng
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The generation of submicrometer-sized particles during dry sliding between stainless steel surfaces is investigated by means of a laser spectrometer for particle counting and scanning tunnelling ...
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    Time-Resolved Vane-Rotor Interaction in a High-Pressure Turbine Stage 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001:;page 1
    Author(s): R. J. Miller; R. W. Moss; R. W. Ainsworth; C. K. Horwood
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper describes the time-varying aerodynamic interaction mechanisms that have been observed within a transonic high-pressure turbine stage; these are inferred from the time-resolved behavior ...
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    Flight and Propulsion Control Integration for Selected In-Flight Thrust Vectoring Modes 

    Source: Journal of Engineering for Gas Turbines and Power:;1979:;volume( 101 ):;issue: 001:;page 168
    Author(s): C. J. Yi; R. L. Heimbold; R. J. Miller; E. Rachovitsky
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The synthesis of a flight control system for an advanced air-superiority fighter equipped with jet flaps, and its flight simulator performance, is reported in this paper. Several control modes ...
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    Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part I: Vane-Rotor and Rotor-Vane Interaction 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001:;page 33
    Author(s): R. J. Miller; R. W. Moss; R. W. Ainsworth; N. W. Harvey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The composition of the time-resolved surface pressure field around a high-pressure rotor blade caused by the presence of neighboring blade rows is investigated, with the individual effects of ...
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    Wake, Shock, and Potential Field Interactions in a 1.5 Stage Turbine—Part II: Vane-Vane Interaction and Discussion of Results 

    Source: Journal of Turbomachinery:;2003:;volume( 125 ):;issue: 001:;page 40
    Author(s): R. J. Miller; R. W. Moss; R. W. Ainsworth; N. W. Harvey
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: The composition of the time-resolved surface pressure field around a high-pressure rotor blade caused by the presence of neighboring blade rows is investigated with the individual effects of ...
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