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Showing 1 to 11 of 11 for “"Three-Dimensional Separation"”.

  1. Experimental and Numerical Study of Endwall Film Cooling

    … the location of the saddle point and the three-dimensional separation lines. Computational predictions showed that the leading-edge horseshoe vortex was confined to approximately 1.5% of the airfoil span for the no film injection case and intensified with low momentum film injection. At …

    ucf

  2. Active and passive separation control for drag reduction of a maneuvering hull form

    Boundary layer separation is a source of large fluid dynamic forces on many engineered vehicles and structures, limiting the speed and efficiency at which we transport people and goods. The maneuvering of ocean and air vehicles in particular is limited by resistance due to cross-flow separation. …

    mit Repository record for Active and passive separation control for drag reduction of a maneuvering hull form (opens in a new tab)

  3. Separation and wakes over three-dimensional bodies

    … was visualized with dyes. The measurement of three-dimensional boundary layers required a special design of the laser optics. Attention was focused in the neighborhood of three-dimensional separation. The Vortex-Lattice method was employed to calculate the inviscid flow and the development of …

    vt Repository record for Separation and wakes over three-dimensional bodies (opens in a new tab)

  4. The Impact of Three Dimensional Flow Anisotropy and Transients on Turbulence Ingestion Noise in Open Rotors

    The effect of flow anisotropy and three dimensional separation on the turbulent structure and radiated turbulence ingestion noise of a rotor in two experimental configurations is studied. The first consists of a non-axisymmetric boundary layer wake ingested by a rotor mounted at the aft of a body …

    vt Repository record for The Impact of Three Dimensional Flow Anisotropy and Transients on Turbulence Ingestion Noise in Open Rotors (opens in a new tab)

  5. A simple criterion for three-dimensional flow separation in axial compressors

    … the estimation, control and mitigation of three-dimensional separation near the hub corner in axial- flow compressors. A simple method to estimate the onset of hub comer separation in compressor blade passages has been developed. A parameter is defined to quantify the combined effect of …

    mit Repository record for A simple criterion for three-dimensional flow separation in axial compressors (opens in a new tab)

  6. Aeroacoustic transfer of leading edge serrations from single aerofoils to low-pressure fan applications

    … are found to be responsible for a complex three-dimensional separation mechanism of the leading edge serrations, causing a delay of stall. The generated data basis is then used to design low-pressure axial fans of minimum complexity by keeping the initially chosen aerofoil type. The …

    tu-berlin Repository record for Aeroacoustic transfer of leading edge serrations from single aerofoils to low-pressure fan applications (opens in a new tab)

  7. Sturcture of Three-Dimensional Separated Flow on Symmetric Bumps

    … x/H Â¥ 3.26 for each case. Complex vortical separations occur on the leeside and merge into large stream-wise mean vortices downstream for the 2 axisymmetric cases. The near-wall flow (y+ < 90) is dominated by the wall. For the axisymmetric cases, the vortices in the outer region produce …

    vt Repository record for Sturcture of Three-Dimensional Separated Flow on Symmetric Bumps (opens in a new tab)

  8. Towards Predictive Eddy Resolving Simulations for Gas Turbine Compressors

    … to prevent dispersion. On the suction surface, separation induced transition occurs. The flow here is seen to be relatively insensitive to numerical smoothing and the choice of SGS model, as long as the Smagorinsky-Lilly SGS model is not used. These findings are encouraging, as they show that, …

    cambridge Repository record for Towards Predictive Eddy Resolving Simulations for Gas Turbine Compressors (opens in a new tab)

  9. Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade

    … the results from an experimental study of three-dimensional turbulent tip gap flow in a linear cascade wind tunnel with 3.3% chord tip clearance with and without moving endwall simulation. Experimental measurements have been completed in Virginia Tech low speed linear cascade wind tunnel. A …

    vt Repository record for Near Wall Behavior of Vortical Flow around the Tip of an Axial Pump Rotor Blade (opens in a new tab)

  10. The effects of pressure waves on turbulent oblique shock wave boundary layer interactions in rectangular channels

    … separates further upstream than the primary separation and displaces the incoming flow. This generates corner compression and expansion waves which propagate into the primary interaction. Previous investigations have examined the effects of corner pressure waves on the interaction with the …

    cambridge Repository record for The effects of pressure waves on turbulent oblique shock wave boundary layer interactions in rectangular channels (opens in a new tab)

  11. An Experimental Spatio-Temporal Analysis of Separated Flows Over Bluff Bodies Using Quantitative Flow Visualization

    In order to study three-dimensional unsteady turbulent flow fields such as the wakes of bluff bodies, a Digital Particle Image Velocimetry (DPIV) system was developed. This system allows non-intrusive two-dimensional and time varying velocity measurements. Software and hardware modifications …

    vt Repository record for An Experimental Spatio-Temporal Analysis of Separated Flows Over Bluff Bodies Using Quantitative Flow Visualization (opens in a new tab)