Global ETD Search

Search theses and dissertations gathered from participating repositories worldwide. Every result links back to the library that holds it. No account is needed.

Results

Showing 1 to 12 of 12 for “"blade heat transfer"”.

  1. Effects of freestream turbulence on turbine blade heat transfer in transonic flow

    … grid generated freestream turbulence on surface heat transfer to turbine blades were measured experimentally. Time-resolved and unsteady heat flux measurements were made with Heat Flux Microsensors at two positions on the suction side of turbine blades. The experiments were conducted on a …

    vt Repository record for Effects of freestream turbulence on turbine blade heat transfer in transonic flow (opens in a new tab)

  2. Turbine Blade Heat Transfer Measurements in a Transonic Flow Using Thin Film Gages

    Experimental heat transfer data has been collected at engine representative conditions in this work to use in future work to improve computational models. Tests were carried out in a transonic cascade wind tunnel with the data collected using thin film gages. All of the necessary development to use …

    vt Repository record for Turbine Blade Heat Transfer Measurements in a Transonic Flow Using Thin Film Gages (opens in a new tab)

  3. Effects of stationary wake on turbine blade heat transfer in a transonic cascade

    … by a stationary upstream strut on surface heat transfer to turbine blades were measured experimentally. Time-resolved and unsteady heat flux measurements were made with Heat Flux Microsensors (HFM) at three positions on the suction surface and one position on the pressure surface of a …

    vt Repository record for Effects of stationary wake on turbine blade heat transfer in a transonic cascade (opens in a new tab)

  4. Effects of shock wave passing on turbine blade heat transfer in a transonic turbine cascade

    The effects of a shock wave passing through a blade passage on surface heat transfer to turbine blades were measured experimentally. The experiments were performed in a transonic linear cascade which matched engine Reynolds number, Mach number, and shock strength. Unsteady heat flux measurements …

    vt Repository record for Effects of shock wave passing on turbine blade heat transfer in a transonic turbine cascade (opens in a new tab)

  5. Effects of Freestream Turbulence, Turbulence Length Scale, and Reynolds Number on Turbine Blade Heat Transfer in a Transonic Cascade

    … scale, and exit Reynolds number on the surface heat transfer distribution of a turbine blade at realistic engine Mach numbers. Passive turbulence grids were used to generate freestream turbulence levels of 2%, 12%, and 14% at the cascade inlet. The turbulence grids produced length scales …

    vt Repository record for Effects of Freestream Turbulence, Turbulence Length Scale, and Reynolds Number on Turbine Blade Heat Transfer in a Transonic Cascade (opens in a new tab)

  6. Impact of aerothermal modeling on the estimation of turbine blade life

    … of aerothermal modeling on estimates of turbine blade heat transfer and life was assessed for three high pressure turbine blades. The work was conducted as part of a project aimed at the evaluation of the effect of variability on turbine life. Pressure and thermal loads were extracted from …

    mit Repository record for Impact of aerothermal modeling on the estimation of turbine blade life (opens in a new tab)

  7. The Development of an Accelerated Testing Facility for the Study of Deposits in Land-Based Gas Turbine Engines

    … on many parameters related to fluid dynamics and heat transfer. Many of these parameters change dynamically once the engine enters service and begins to experience surface degradation. This thesis presents a validation of the design and operation of an accelerated testing facility for the study of …

    byu Repository record for The Development of an Accelerated Testing Facility for the Study of Deposits in Land-Based Gas Turbine Engines (opens in a new tab)

  8. Effects of High Intensity, Large-Scale Freestream Combustor Turbulence On Heat Transfer in Transonic Turbine Blades

    … combustor and first stage vane on turbine blade heat transfer has been measured and analytically modeled in a linear, transonic turbine cascade. Measurements were performed on a high turning, transonic turbine blade. The facility is capable of heated flow with inlet total temperature of …

    vt Repository record for Effects of High Intensity, Large-Scale Freestream Combustor Turbulence On Heat Transfer in Transonic Turbine Blades (opens in a new tab)

  9. Experimental and Computational Study of Heat Transfer on a Turbine Blade Tip with a Shelf

    … materials. The gap between rotating turbine blades and the stationary shroud provides an unintended flow path for hot gases. Gases that flow through the tip region cause pressure losses in the turbine section and high heat loads to the blade tip. This thesis studies the heat transfer on an …

    vt Repository record for Experimental and Computational Study of Heat Transfer on a Turbine Blade Tip with a Shelf (opens in a new tab)

  10. Comparison of the Thermal Performance of Several Tip Cooling Designs for a Turbine Blade

    Gas turbine blades are subject to harsh operating conditions that require innovative cooling techniques to insure reliable operation of parts. Film-cooling and internal cooling techniques can prolong blade life and allow for higher engine temperatures. This study examines several unique methods of …

    vt Repository record for Comparison of the Thermal Performance of Several Tip Cooling Designs for a Turbine Blade (opens in a new tab)

  11. Measurements of Cooling Effectiveness Along the Tip of a Turbine Blade

    In a gas turbine engine, turbine blades are exposed to temperatures above their melting point. Film-cooling and internal cooling techniques can prolong blade life and allow for higher engine temperatures. This study examines a novel cooling technique called a microcircuit, which combines internal …

    vt Repository record for Measurements of Cooling Effectiveness Along the Tip of a Turbine Blade (opens in a new tab)

  12. Film Cooling Predictions Along the Tip and Platform of a Turbine Blade

    … typically exceeding the melting point of the blade material. Cooling methods investigated in this computational study included parasitic cooling flow losses, which are inherent to engines, and microcircuit channels. Parasitic losses included dirt purge holes, located along the blade tip, and …

    vt Repository record for Film Cooling Predictions Along the Tip and Platform of a Turbine Blade (opens in a new tab)