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    What Sets Proficient and Expert Users Apart? Results of a Computer-Aided Design Experiment 

    Source: Journal of Mechanical Design:;2023:;volume( 146 ):;issue: 001:;page 11401-1
    Author(s): Deng, Yuanzhe; Chen, James; Olechowski, Alison
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: As computer-aided design (CAD) tools have become an essential aspect of modern mechanical engineering design, the demand for CAD experts has increased significantly. The development from novice, to proficient, to expert ...
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    Morphing Continuum Theory: Incorporating the Physics of Microstructures to Capture the Transition to Turbulence Within a Boundary Layer 

    Source: Journal of Fluids Engineering:;2017:;volume( 139 ):;issue: 001:;page 11205
    Author(s): Wonnell, Louis B.; Chen, James
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: A boundary layer with Re = 106 is simulated numerically on a flat plate using morphing continuum theory. This theory introduces new terms related to microproperties of the fluid. These terms are added to a finite-volume ...
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    Boltzmann–Curtiss Description for Flows Under Translational Nonequilibrium 

    Source: Journal of Fluids Engineering:;2020:;volume( 142 ):;issue: 005
    Author(s): Ahmed, Mohamed M.; Cheikh, Mohamad I.; Chen, James
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Continuum-based theories, such as Navier–Stokes (NS) equations, have been considered inappropriate for flows under nonequilibrium conditions. In part, it is due to the lack of rotational degrees-of-freedom in the ...
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    Degraded Planary Tracking Control of an Omnidirectional Vectored-Thruster Aerostat 

    Source: Journal of Aerospace Engineering:;2019:;Volume (032):;issue:004
    Author(s): Li Chen;James F. Whidborne;Qi Dong;Dengping Duan;Jinguo Liu
    Publisher: American Society of Civil Engineers
    Abstract: The problem of horizontal-plane tracking control of an omnidirectional, four vectored-thruster aerostat subjected to actuator failure is considered. The actuator failures result in the aerostat’s becoming underactuated, ...
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    DSpace software copyright © 2002-2015  DuraSpace
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