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    On Boundary-Layer Stabilization by Bio-Inspired Compliant Coatings for Underwater Drones

    Source: Journal of Fluids Engineering:;2026:;volume( 148 ):;issue:006::page 31
    Author:
    Das, Debayan
    ,
    Schrader, Lars-Uve
    DOI: 10.1115/1.4071254
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: Abstract. The advent of unmanned underwater vehicles (UUVs) has enabled scientific research, resource exploration, and infrastructure development at the depths of the oceans. At such depths (>100 m), with freestream turbulence intensity Tu<1.5 %, predominant drag component on a streamlined UUV is the skin friction drag. Inspired by dolphin skin, we propose a two-layer silicone-based compliant coating comprising a thick blubber that undergoes wall-normal compression, and a thin dermis that undergoes bending deformation. For the proposed choice of material and coating parameters, the energy exchange at the wall, due to deformation of the compliant surface, serves to attenuate the growth of Tollmien–Schlichting (TS) waves. This stabilizing effect of the compliant surface allows the vehicle to maintain low-drag laminar boundary-layer flow over a greater portion of the wetted surface. The efficacy of the proposed coating has been studied on the X-35 UUV in this work. Numerical simulations of the flow around this UUV have been performed at a cruise Reynolds number ReL=1.185×107, using pisofoam to characterize the boundary layer. The Falkner–Skan solution with wedge angle βw=24.8deg was found to be a close approximation of the fore-body laminar boundary layer. Using this self-similar baseflow, the Orr–Sommerfeld equation was solved with compliant wall boundary conditions to compute the amplification of TS waves. For the best-performing coating, with blubber thickness hB=7 mm, the transition point shifts from 18% to 47% of the UUV length, without triggering any fluid-induced surface instabilities (FISI). This delay in laminar-to-turbulent transition allows for potentially 31% reduction in skin-friction drag on the UUV.
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      On Boundary-Layer Stabilization by Bio-Inspired Compliant Coatings for Underwater Drones

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    https://yetl.yabesh.ir/yetl1/handle/yetl/4314780
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    contributor authorDas, Debayan
    contributor authorSchrader, Lars-Uve
    date accessioned2026-08-23T07:12:52Z
    date available2026-08-23T07:12:52Z
    date copyright2026/06/01
    date issued2026
    identifier issn0098-2202
    identifier otherfe-25-1536.pdf
    identifier urihttp://yetl.yabesh.ir/yetl1/handle/yetl/4314780
    description abstractAbstract. The advent of unmanned underwater vehicles (UUVs) has enabled scientific research, resource exploration, and infrastructure development at the depths of the oceans. At such depths (>100 m), with freestream turbulence intensity Tu<1.5 %, predominant drag component on a streamlined UUV is the skin friction drag. Inspired by dolphin skin, we propose a two-layer silicone-based compliant coating comprising a thick blubber that undergoes wall-normal compression, and a thin dermis that undergoes bending deformation. For the proposed choice of material and coating parameters, the energy exchange at the wall, due to deformation of the compliant surface, serves to attenuate the growth of Tollmien–Schlichting (TS) waves. This stabilizing effect of the compliant surface allows the vehicle to maintain low-drag laminar boundary-layer flow over a greater portion of the wetted surface. The efficacy of the proposed coating has been studied on the X-35 UUV in this work. Numerical simulations of the flow around this UUV have been performed at a cruise Reynolds number ReL=1.185×107, using pisofoam to characterize the boundary layer. The Falkner–Skan solution with wedge angle βw=24.8deg was found to be a close approximation of the fore-body laminar boundary layer. Using this self-similar baseflow, the Orr–Sommerfeld equation was solved with compliant wall boundary conditions to compute the amplification of TS waves. For the best-performing coating, with blubber thickness hB=7 mm, the transition point shifts from 18% to 47% of the UUV length, without triggering any fluid-induced surface instabilities (FISI). This delay in laminar-to-turbulent transition allows for potentially 31% reduction in skin-friction drag on the UUV.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleOn Boundary-Layer Stabilization by Bio-Inspired Compliant Coatings for Underwater Drones
    typeJournal Paper
    journal volume148
    journal issue6
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4071254
    journal fristpage31
    journal lastpage48
    page18
    treeJournal of Fluids Engineering:;2026:;volume( 148 ):;issue:006
    contenttypeFulltext
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    DSpace software copyright © 2002-2015  DuraSpace
    نرم افزار کتابخانه دیجیتال "دی اسپیس" فارسی شده توسط یابش برای کتابخانه های ایرانی | تماس با یابش
    yabeshDSpacePersian