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Showing 1 to 20 of 42 for “"Strouhal number"”.

  1. Maneuvering of a robotic pike

    … are quantified and analyzed. A non-dimensional number, the Maneuvering Strouhal Number (Stm) is defined based on observations from live fish and previous theoretical developments. Recommendations for further improvements in the maneuvering performance of flexible hull vehicles are derived based …

    mit Repository record for Maneuvering of a robotic pike (opens in a new tab)

  2. Blade tonal noise reduction using tail articulation at high Reynolds number

    … freestream velocities corresponding to Reynolds number in the range 75,000 < Re < 300,000 and (ii) operate at frequencies up to 30 Hz in order to investigate the range of Strouhal number 0.0 < St < 0.35. Velocity measurements in the active stator wake are carried out by Laser Doppler Velocimetry, …

    mit Repository record for Blade tonal noise reduction using tail articulation at high Reynolds number (opens in a new tab)

  3. Performance of biologically inspired flapping foils

    … fashion. The effects of varying Reynolds number, Strouhal number, maximum pitch angle, and the phase shift between heave and pitch were studied. It was determined that at very low Strouhal numbers the wake was 'S' like and at moderate Strouhal numbers the wake contained discreet …

    mit Repository record for Performance of biologically inspired flapping foils (opens in a new tab)

  4. Reduction of unsteady underwater propeller forces via active tail articulation

    … stator model. Tests were conducted at a Reynolds number of 75,000 and stator tail articulation was carried out in the range of Strouhal number 0.0 < St < 0.13. A variety of non-lifting propellers were used to investigate sinusoidal articulation profiles in the range of am- plitudes (2°,5°,10°), …

    mit Repository record for Reduction of unsteady underwater propeller forces via active tail articulation (opens in a new tab)

  5. The Influence of Trailing Edge Shape and Kinematics on Bio-inspired Pitching Panels

    … in a systematic manner at moderate Reynolds number. The wakes behaviors and wake dynamics of these panels are explored in a time-varying and time-averaged sense using results obtained from multiple planes of stereoscopic particle image velocimetry. The time-averaged and time-varying …

    syracuse-diss Repository record for The Influence of Trailing Edge Shape and Kinematics on Bio-inspired Pitching Panels (opens in a new tab)

  6. Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape

    … shedding from the separation bubble. The average Strouhal number of this regular mode corresponded to StL = 0.60, and the average vortex convection velocity was observed to be 0.45U∞. These values were highly consistent with those reported elsewhere in the literature. The other two frequencies …

    uiuc Repository record for Unsteady modes in the flowfield about an airfoil with a leading-edge horn-ice shape (opens in a new tab)

  7. Three-dimensional vortical structures in the wake of a flexible flapping foil

    … of a flexible flapping foil at Reynolds number 164. Flexible foils were fabricated, coated with fluorescent dye, and towed with heave and pitch in a large glass tank. The foil cross section is a NACA 0030 foil shape, and the foil has an aspect ratio of 3. Pictures where taken of the …

    mit Repository record for Three-dimensional vortical structures in the wake of a flexible flapping foil (opens in a new tab)

  8. Study of Steady and Pulsating Impinging Jets

    … diameters in length.The effects of the Reynolds number, the nozzle-to-plate spacing and the Strouhal number were investigated systematically. The range of the Reynolds numbers covered is 4000 to 10000 for the steady jets, and 4200 to 10240 for the pulsed jets. The nozzle-to-plate spacings …

    qu-belfast Repository record for Study of Steady and Pulsating Impinging Jets (opens in a new tab)

  9. Study of flow past elliptic and circular cylinders using direct numerical simulation

    … it is found that important quantities like the Strouhal number and lift and drag coefficients match well with established values.

    uiuc Repository record for Study of flow past elliptic and circular cylinders using direct numerical simulation (opens in a new tab)

  10. Etude expérimentale des sons auto-entretenus produits par un jet issu d'un conduit et heurtant une plaque fendue

    … tones (up to 125 dB) by a low Mach number free plane jet impinging on a slotted plate, known as slot-tone, is experimentally studied. For all geometries of the slot’s edge tested, the tones are generated from 6 m/s and when a resonant mode of the duct from which the jet flows out is …

    liege Repository record for Etude expérimentale des sons auto-entretenus produits par un jet issu d'un conduit et heurtant une plaque fendue (opens in a new tab)

  11. Structure and Dynamics of a Reacting Jet Injected into a Vitiated Crossflow in a Staged Combustion System

    … with the reacting jet in crossflow. The wake Strouhal number calculation provides a better physical insight into the influence of jet velocity profile and nature of crossflow. A decrease in wake Strouhal number is noticed with an increase in nozzle separation distance. The effect of near-field …

    purdue-thes Repository record for Structure and Dynamics of a Reacting Jet Injected into a Vitiated Crossflow in a Staged Combustion System (opens in a new tab)

  12. Assessment of Formulations for Numerical Solutions of Low Speed, Unsteady, Turbulent Flows over Bluff Bodies

    … aerodynamic forces, mean pressure coefficient, Strouhal number, mean velocity magnitude and turbulence intensity. The main results can be summarized as follows. First, the predictions are more sensitive to the turbulence model choice than to the choice of algorithm. The Spalart-Allmaras model …

    vt Repository record for Assessment of Formulations for Numerical Solutions of Low Speed, Unsteady, Turbulent Flows over Bluff Bodies (opens in a new tab)

  13. Nonlinear electrokinetic transport and its applications under combined AC and DC fields in micro/nanofluidic interface devices

    … greater than the DC voltage and at low Strouhal number, results in large dual concentration polarization regions (with unequal lengths) at both the micro/nanofluidic interfaces due to large and unequal voltage drops at these junctions. The highly nonlinear potential distribution gives …

    uiuc Repository record for Nonlinear electrokinetic transport and its applications under combined AC and DC fields in micro/nanofluidic interface devices (opens in a new tab)

  14. Dynamical systems analysis of electrostatic and aerodynamic forced vibrations of a thin flexible electrode

    … 0.224 - 3.58 m/s (0.5 - 8 mile/hr). The Reynolds numbers for these speeds lie in the range of 1000 - 20000. A range of control parameters leading to stable vibrations are established using the Strouhal number as the operating parameter whose inverse values change from 100 - 2500. The Numerical …

    iastate Repository record for Dynamical systems analysis of electrostatic and aerodynamic forced vibrations of a thin flexible electrode (opens in a new tab)

  15. Investigating the Effect of an Upstream Spheroid on Tandem Hydrofoils

    … data. The simulations were run for a range of Strouhal numbers (0.2-0.5) and phase differences (0-π). Results were compared to identical simulations without an upstream body to determine how the body affects thrust generation and the unsteady flow field.</p> <p>The combined time-averaged thrust …

    calpoly Repository record for Investigating the Effect of an Upstream Spheroid on Tandem Hydrofoils (opens in a new tab)

  16. Large eddy simulation of acoustic propagation in turbulent flow through ducts and mufflers

    … solver is developed and validated for a low Mach number flow simulation of acoustic pulse. This new solver is developed using C++ based OpenFOAM toolkit and further tested for low Mach number flow test case. The analysis of simple expansion muffler for various structures, frequency ranges and …

    hull Repository record for Large eddy simulation of acoustic propagation in turbulent flow through ducts and mufflers (opens in a new tab)

  17. Experimental studies of flapping foils for energy extraction

    … sinusoidially 90° out of phase at a Reynolds number of 13,800. Energy extraction efficiencies of up to [eta] = 0.45 were found within a very small parametric region for small oscillation amplitudes while broad regions of appreciable efficiency were found at large oscillation amplitudes. The …

    mit Repository record for Experimental studies of flapping foils for energy extraction (opens in a new tab)

  18. Wall-Jet Turbulence and Mixing Control by Way of a Pulsed Inlet Velocity

    … the wall-normal turbulence intensity at a Strouhal number (Sr) of 0.05 and reduces the turbulence intensity in all directions at a Sr of 0.25. The incompressible wall-jet simulations show that a perturbation of magnitude 40% of the inlet velocity at a low Sr number of 0.0048 damps …

    embry-riddle Repository record for Wall-Jet Turbulence and Mixing Control by Way of a Pulsed Inlet Velocity (opens in a new tab)

  19. A Reduced-Order Model Bi-Modal Excitation of a Supersonic Planar Jet

    … excitation is then examined for the fundamental Strouhal number 0.10, which has been identified as a dominant noise source. Cases were considered separately with adding the subharmonic and the harmonic as a means of reducing the amplitude of the fundamental. Adding the subharmonic had minimal …

    embry-riddle Repository record for A Reduced-Order Model Bi-Modal Excitation of a Supersonic Planar Jet (opens in a new tab)

  20. Transition from laminar to turbulent flow around an airfoil

    … an airfoil of arbitrary shape. A low-Reynolds-number k — e turbulence model including curvature effect was used to consider the gain and loss of turbulent kinetic energy. To include laminar sublayer into the computational domain, a multi-layer grid and a cubic-slpine grid were introduced …

    must-thes Repository record for Transition from laminar to turbulent flow around an airfoil (opens in a new tab)

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