2010
DOI: 10.2514/1.43389
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Computations of Flapping Flow Propulsion for Unmanned Underwater Vehicle Design

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Cited by 16 publications
(9 citation statements)
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“…An unstructured grid-based unsteady incompressible Navier-Stokes solver with automatic adaptive remeshing was used to compute the flow about the deforming fins through several cycles of oscillation. We have validated our computational tools and Ramamurti et al 3 have demonstrated the capability of the pectoral fins on a four fin propelled UUV 4 . In order to increase the thrust generated by the fins and to increase the payload capacity, a larger vehicle is developed.…”
Section: Introductionmentioning
confidence: 68%
“…An unstructured grid-based unsteady incompressible Navier-Stokes solver with automatic adaptive remeshing was used to compute the flow about the deforming fins through several cycles of oscillation. We have validated our computational tools and Ramamurti et al 3 have demonstrated the capability of the pectoral fins on a four fin propelled UUV 4 . In order to increase the thrust generated by the fins and to increase the payload capacity, a larger vehicle is developed.…”
Section: Introductionmentioning
confidence: 68%
“…Fixing the fin root at a specific angle deviates from nature, but the construction simplicity and cost savings are so substantial that some performance penalty was accepted. The flapping stroke amplitude and frequency, as well as the phasing of the individual fin tip deflection time histories, were retained as controllable parameters, and we have performed CFD analyses of force production with this fin configuration (Ramamurti et al, 2010).…”
Section: Figurementioning
confidence: 99%
“…Hardware control and all computations are performed by a 16-MHz ATmega2560 microcontroller. Computations (Ramamurti et al, 2010) and experimental tests carried out to date (Geder et al, 2011) characterized how changes in fin stroke amplitude, frequency, bias angle, and curvature affect the thrust and lift forces for zero free stream flow speed. Further testing and computations are ongoing to fully characterize the fin forces and vehicle dynamics.…”
Section: Figurementioning
confidence: 99%
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“…We have validated our computational tools 10 and demonstrated the capability of the pectoral fins on a four fin propelled UUV 11 . In order to increase the 2 American Institute of Aeronautics and Astronautics thrust generated by the fins and to increase the payload capacity, a larger vehicle is developed.…”
Section: Introductionmentioning
confidence: 97%