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Showing 1 to 20 of 108 for “"Secondary Flow"”.

  1. Electrohydrodynamic Secondary Flow

    Made available in DSpace on 2015-05-12T21:43:43Z (GMT). No. of bitstreams: 2 license.txt: 4848 bytes, checksum: 96035ab3f5e1c23cc7138a224ce498bd (MD5) 6915365.PDF: 17343384 bytes, checksum: d54b8d43ba0b40c091be52e796088c9c (MD5) Previous issue date: 1969

    uiuc Repository record for Electrohydrodynamic Secondary Flow (opens in a new tab)

  2. Secondary flow in axial compressors

    Thesis (Sc.D.) Massachusetts Institute of Technology. Dept. of Mechanical Engineering, 1954.

    mit Repository record for Secondary flow in axial compressors (opens in a new tab)

  3. The secondary flow in rectangular ducts

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1957.

    mit Repository record for The secondary flow in rectangular ducts (opens in a new tab)

  4. Secondary flow heat transfer phenomena in branch piping

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1983.

    mit Repository record for Secondary flow heat transfer phenomena in branch piping (opens in a new tab)

  5. A secondary flow approach to the inlet vortex flow field

    … with the vortex is investigated using a secondary flow approach. In this approach the flow is assumed to be composed of an irrotational primary flow and a weak shear flow, with the vortex filaments associated with the latter being regarded as convected by the former. The potential flow

    mit Repository record for A secondary flow approach to the inlet vortex flow field (opens in a new tab)

  6. Improving the performance of aerofoil sections using momentum transfer via a secondary flow

    Aerodynamic flow control can improve aerofoil performance by influencing the natural growth of boundary layers, which develop on the surface of vehicles moving in viscous fluids. Many active and passive techniques have been developed to reduce drag and/or increase the lift of aerofoil …

    southwales Repository record for Improving the performance of aerofoil sections using momentum transfer via a secondary flow (opens in a new tab)

  7. Detection of secondary flow in a turbine cascade using a tracer gas technique

    This thesis presents an investigation into the motions of the horseshoe vortices and the passage vortex, within a plane turbine blade cascade. Fluid motion was determined using a tracer gas technique. Ethylene was injected into the pressure-side and suction-side legs of the horseshoe vortex, near …

    vt Repository record for Detection of secondary flow in a turbine cascade using a tracer gas technique (opens in a new tab)

  8. Reduction of Secondary Flow Losses in a Turbine for Use in Man-Portable Power Generation

    … is on the turbine components and how the secondary flow losses from the generated airfoil shapes can be reduced to improve component performance. One of the secondary flow loss items to be addressed is the generation of the Horseshoe Vortex. The Horseshoe Vortex is an aerodynamic …

    embry-riddle Repository record for Reduction of Secondary Flow Losses in a Turbine for Use in Man-Portable Power Generation (opens in a new tab)

  9. Investigation of the Effects of an Upstream Cavity on the Secondary Flow in Transonic Turbine Blade Passages with Endwall Contouring

    … here aims to contribute to the understanding of secondary flows in modern high-pressure (HP) turbine blade passages. More specifically, it aims to improve the understanding of vortical structures near the endwall with respect to the presence of an upstream cavity that approximates the gap present …

    carleton Repository record for Investigation of the Effects of an Upstream Cavity on the Secondary Flow in Transonic Turbine Blade Passages with Endwall Contouring (opens in a new tab)

  10. Liquid metal brushes for homopolar devices

    … require a thorough knowledge of liquid metal flows in a narrow gap between a fixed surface and a moving surface, with a strong applied magnetic field and with a free surface beyond each moving end of the gap. The radial and axial velocities in the secondary flow are reduced by a strong axial …

    uiuc Repository record for Liquid metal brushes for homopolar devices (opens in a new tab)

  11. The influence of channel-skewed bedforms on flow structure in a high-amplitude meandering channel

    The interaction of flow, sediment transport, and substrate morphology (morphodynamics) leads to complex boundary configurations of ripples, dunes, and bars along alluvial rivers. The instantaneous boundary morphology heavily influences the local flow structure, especially within meander bends, and …

    uiuc Repository record for The influence of channel-skewed bedforms on flow structure in a high-amplitude meandering channel (opens in a new tab)

  12. Effects of Tip Clearance and Surface Roughness on Small-Scale Turbopump Impeller Performance

    … turbopump impellers by assessing the dominant flow features, quantifying the underlying loss mechanisms, and determining the sensitivity of performance losses to changes in tip clearance and surface roughness. The study identifies the primary flow features governing impeller performance to be …

    mit Repository record for Effects of Tip Clearance and Surface Roughness on Small-Scale Turbopump Impeller Performance (opens in a new tab)

  13. Experimental and numerical modeling of submarine channel flow and morphodynamics

    … are recognized as products of density-driven flows known as turbidity currents. The flow field and the morphodynamics of these channels, however, remain poorly understood due to dormancy of these systems during the present geologic time. Both laboratory and numerical modeling allow the study …

    south-carolina Repository record for Experimental and numerical modeling of submarine channel flow and morphodynamics (opens in a new tab)

  14. Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions with and without Blowing

    … to improve aerodynamic performance by reducing secondary flow strength. The effects of endwall contouring with discrete holes and an upstream purge slot for a high turning (127") airfoil passage under transonic conditions are investigated. The total pressure loss and secondary flow field were …

    vt Repository record for Aerodynamics of Endwall Contouring with Discrete Holes and an Upstream Purge Slot Under Transonic Conditions with and without Blowing (opens in a new tab)

  15. Effect of width-to-depth ratio on the mean flow velocities for a Kinoshita meander bend

    … a Kinoshita meander bend. The characteristics of flow in such a bend have been studied by Ancalle (2007) and Abad and Garcia (2009a) for width-to-depth ratios equal to 2.4 and 4.0. The present study extends that work and includes a higher width-to-depth ratio (equal to 12.0) in addition to those …

    uiuc Repository record for Effect of width-to-depth ratio on the mean flow velocities for a Kinoshita meander bend (opens in a new tab)

  16. Non-Intrusive Sensing and Feedback Control of Serpentine Inlet Flow Distortion

    … intensity found in serpentine inlet airflow was established using wall-pressure fluctuation measurements. This sensing technique was experimentally developed for aircraft with serpentine inlets in a symmetric, level flight condition. The turbulence carried by the secondary flow field …

    vt Repository record for Non-Intrusive Sensing and Feedback Control of Serpentine Inlet Flow Distortion (opens in a new tab)

  17. Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine

    … between the combustor and turbine. The flow field at a combustor exit shows non-uniformities in pressure, temperature, and velocity in the pitch and radial directions. This inlet profile to the turbine can have a considerable effect on the development of the secondary flows through the …

    vt Repository record for Flow Field Computations of Combustor-Turbine Interactions in a Gas Turbine Engine (opens in a new tab)

  18. Endwall Heat Transfer and Shear Stress for a Nozzle Guide Vane with Fillets and a Leakage Interface

    … combustor is compounded by a complex vortical secondary flow at the junction of the endwall and the airfoil. This flow tends to increase local heat transfer rates and sweep coolant away from component surfaces, as well as decrease the turbine aerodynamic efficiency. Past research has shown that …

    vt Repository record for Endwall Heat Transfer and Shear Stress for a Nozzle Guide Vane with Fillets and a Leakage Interface (opens in a new tab)

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