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    A Study of Shock-Induced Transient Jets: The Impact of Exit Conditions on Mach Disk and Vortex Ring 

    Source: Journal of Fluids Engineering:;2024:;volume( 146 ):;issue: 008:;page 81202-1
    Author(s): V., Vinod; Rao, Divya; Chandrala, Lakshmana Dora
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: We investigate the effect of exit pressure history on the flow characteristics of underexpanded transient jets. Using both experiments and numerical simulations, we study the dynamics of shock-cell and vortex structures ...
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    Unsteady Wake Characteristics of a Flapping Wing through 3D TR-PIV 

    Source: Journal of Aerospace Engineering:;2012:;Volume ( 025 ):;issue: 004
    Author(s): Saurav Kumar; Ghosh; Chandrala Lakshmana; Dora; Debopam; Das
    Publisher: American Society of Civil Engineers
    Abstract: The unsteady wake characteristics of a butterfly-shaped wing undergoing flapping and feathering motions are studied. A 4-bar quick return mechanism is used to generate the flapping motion. To achieve considerable feathering ...
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    DSpace software copyright © 2002-2015  DuraSpace
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