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Showing 1 to 6 of 6 for “"Rib Turbulators"”.

  1. Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators

    … and walls with 45 degree angled and V-shaped rib turbulators were investigated numerically using an unstructured, incompressible, Reynolds-averaged Navier-Stokes flow solver. The influence of 45 degree angled ribs and channel orientation on the local Nusselt number ratios for leading and …

    utc Repository record for Computation of heat transfer in turbine rotor blade cooling channels with angled rib turbulators (opens in a new tab)

  2. Experiments and simulation of shaped film cooling holes fed by crossflow with rib turbulators

    … crossflow channel. In this study, angled rib turbulators were installed in two geometric configurations inside the internal crossflow channel, at 45° and 135°, to assess the impact on film cooling effectiveness. Film cooling hole inlets positioned in both pre-rib and post-rib locations …

    texas Repository record for Experiments and simulation of shaped film cooling holes fed by crossflow with rib turbulators (opens in a new tab)

  3. Heat Transfer in Stationary and Rotating Coolant Channels Using a Transient Liquid Crystal Technique

    … method, multipass coolant channels with rib turbulators, large diameter radially outward channels with rib turbulators, and jet impingement cooling schemes are studied during rotation. 90deg, W, and M-shaped rib enhancements are studied and detailed heat transfer measurements clearly …

    vt Repository record for Heat Transfer in Stationary and Rotating Coolant Channels Using a Transient Liquid Crystal Technique (opens in a new tab)

  4. Detailed Heat Transfer Measurements of Various Rib Turbulator Shapes at Very High Reynolds Numbers Using Steady-state Liquid Crystal Thermography

    … turbine blades feature serpentine passages where rib turbulators are installed to enhance heat transfer between the relatively colder air bled off from the compressor and the hot internal walls. Most of the prior studies have been restricted to Reynolds number of 90000 and several studies have …

    vt Repository record for Detailed Heat Transfer Measurements of Various Rib Turbulator Shapes at Very High Reynolds Numbers Using Steady-state Liquid Crystal Thermography (opens in a new tab)

  5. Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under Stationary and Rotating Conditions

    … cooled by jet impingement which cross-over the rib turbulators in the feed chamber. The mid-chord section of the turbine airfoils have serpentine passages connected via. 180° bends, and they feature turbulence promotors which enhance the heat exchange rates between the coolant and the internal …

    vt Repository record for Development of Advanced Internal Cooling Technologies for Gas Turbine Airfoils under Stationary and Rotating Conditions (opens in a new tab)

  6. Heat Transfer Performance Improvement Technologies for Hot Gas Path Components in Gas Turbines

    … usually roughened with turbulence promoters like ribs to enhance heat transfer. Though the ribs help in augmenting the heat transfer, they have an associated pressure penalty as well. Therefore, it is important to study the thermal-hydraulic performance of ribbed internal cooling passages. The …

    vt Repository record for Heat Transfer Performance Improvement Technologies for Hot Gas Path Components in Gas Turbines (opens in a new tab)