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    Combined Experimental/Numerical Development of Propulsor Evaluation Capability

    Source: Journal of Fluids Engineering:;2011:;volume( 133 ):;issue: 008::page 81105
    Author:
    Amanda M. Dropkin
    ,
    Stephen A. Huyer
    ,
    Charles Henoch
    DOI: 10.1115/1.4004387
    Publisher: The American Society of Mechanical Engineers (ASME)
    Abstract: This paper presents a method to combine computational fluid dynamics (CFD) modeling with subscale experiments to improve full-scale propulsor performance prediction. Laboratory experiments were conducted on subscale models of the NUWC Light underwater vehicle in the 0.3048 m × 0.3048 m water tunnel located at the Naval Undersea Warfare Center in Newport, Rhode Island. This model included an operational rim-driven ducted post-swirl propulsor. Laser Doppler Velocimetry was used to measure several velocity profiles along the hull. The experimental data were used in this project to validate the CFD models constructed using the commercial CFD software package, Fluent® . Initially, axisymmetric two-dimensional simulations investigated the bare hull, hull only case, and a shrouded body without the propulsor. These models were selected to understand the axisymmetric flow development and investigate methods to best match the propulsor inflow. A variety of turbulence models were investigated and ultimately the numerical and experimental velocity profiles were found to match within 3%. Full 3D flow simulations were then conducted with an operating propulsor and compared with the corresponding subscale experimental data. Finally, simulations were conducted for full-scale tests and compared with actual open-water data. While the open-water data was limited to propulsor rpm and vehicle velocity, the operating advance ratio could be determined as well as the estimated vehicle thrust. This provided a method to utilize CFD/experiments to bridge the gap between subscale and full-scale tests. The predicted open-water advance ratio was 10.3% higher than the experimental value, as compared with the 28% difference previously found from a linear extrapolation of Reynolds number from model scale to full scale. This method was then applied to two different research propulsor geometries and led to agreement between computational and experimental advance ratios on the order of 2%.
    keyword(s): Flow (Dynamics) , Turbulence , Drag (Fluid dynamics) , Water tunnels , Boundary layers , Computational fluid dynamics , Rotors , Vehicles , Blades , Geometry , Stators , Water , Hull , Reynolds number , Modeling , Laser Doppler anemometry , Reynolds-averaged Navier–Stokes equations , Inflow AND Thrust ,
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      Combined Experimental/Numerical Development of Propulsor Evaluation Capability

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    https://yetl.yabesh.ir/yetl1/handle/yetl/146296
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    • Journal of Fluids Engineering

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    contributor authorAmanda M. Dropkin
    contributor authorStephen A. Huyer
    contributor authorCharles Henoch
    date accessioned2017-05-09T00:44:14Z
    date available2017-05-09T00:44:14Z
    date copyrightAugust, 2011
    date issued2011
    identifier issn0098-2202
    identifier otherJFEGA4-27482#081105_1.pdf
    identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/146296
    description abstractThis paper presents a method to combine computational fluid dynamics (CFD) modeling with subscale experiments to improve full-scale propulsor performance prediction. Laboratory experiments were conducted on subscale models of the NUWC Light underwater vehicle in the 0.3048 m × 0.3048 m water tunnel located at the Naval Undersea Warfare Center in Newport, Rhode Island. This model included an operational rim-driven ducted post-swirl propulsor. Laser Doppler Velocimetry was used to measure several velocity profiles along the hull. The experimental data were used in this project to validate the CFD models constructed using the commercial CFD software package, Fluent® . Initially, axisymmetric two-dimensional simulations investigated the bare hull, hull only case, and a shrouded body without the propulsor. These models were selected to understand the axisymmetric flow development and investigate methods to best match the propulsor inflow. A variety of turbulence models were investigated and ultimately the numerical and experimental velocity profiles were found to match within 3%. Full 3D flow simulations were then conducted with an operating propulsor and compared with the corresponding subscale experimental data. Finally, simulations were conducted for full-scale tests and compared with actual open-water data. While the open-water data was limited to propulsor rpm and vehicle velocity, the operating advance ratio could be determined as well as the estimated vehicle thrust. This provided a method to utilize CFD/experiments to bridge the gap between subscale and full-scale tests. The predicted open-water advance ratio was 10.3% higher than the experimental value, as compared with the 28% difference previously found from a linear extrapolation of Reynolds number from model scale to full scale. This method was then applied to two different research propulsor geometries and led to agreement between computational and experimental advance ratios on the order of 2%.
    publisherThe American Society of Mechanical Engineers (ASME)
    titleCombined Experimental/Numerical Development of Propulsor Evaluation Capability
    typeJournal Paper
    journal volume133
    journal issue8
    journal titleJournal of Fluids Engineering
    identifier doi10.1115/1.4004387
    journal fristpage81105
    identifier eissn1528-901X
    keywordsFlow (Dynamics)
    keywordsTurbulence
    keywordsDrag (Fluid dynamics)
    keywordsWater tunnels
    keywordsBoundary layers
    keywordsComputational fluid dynamics
    keywordsRotors
    keywordsVehicles
    keywordsBlades
    keywordsGeometry
    keywordsStators
    keywordsWater
    keywordsHull
    keywordsReynolds number
    keywordsModeling
    keywordsLaser Doppler anemometry
    keywordsReynolds-averaged Navier–Stokes equations
    keywordsInflow AND Thrust
    treeJournal of Fluids Engineering:;2011:;volume( 133 ):;issue: 008
    contenttypeFulltext
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