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 20 of 203 for “"Vane"”.

  1. Rotating Vane Flow Measurement Techniques

    … into the development and performance of vane flowmeter methods for the measurement of air and gas flow. To improve on existing rotating vane anemometer performance, a capacitance change vane sensing technique is investigated. In conjunction with Ower's dynamic equations steady state and …

    southwales Repository record for Rotating Vane Flow Measurement Techniques (opens in a new tab)

  2. Investigation Into Flutter of Complex Vane Packs

    … in different distortion patterns, the StreamVane and ScreenVane systems have been developed. A StreamVane consists of a complex vane pack that is custom designed for each distortion profile and the ScreenVane combines the StreamVane with a pressure distortion screen for testing engines under …

    vt Repository record for Investigation Into Flutter of Complex Vane Packs (opens in a new tab)

  3. The effects of manufacturing variability on turbine vane performance

    Gas turbine vanes have airfoil shapes optimized to deliver specific flow conditions to turbine rotors. The limitations of the manufacturing process with regards to accuracy and precision mean that no vane will exactly match the design intent. This research effort is an investigation of the effects …

    mit Repository record for The effects of manufacturing variability on turbine vane performance (opens in a new tab)

  4. Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1989.

    mit Repository record for Enhanced compressor distortion tolerance using asymmetric inlet guide vane stagger (opens in a new tab)

  5. 2D CFD Simulation of a Circulation Control Inlet Guide Vane

    … studies of a circulation control Inlet Guide Vane (IGV) that takes advantage of the Coanda effect for flow vectoring. The IGV in this thesis is an uncambered airfoil that alters circulation around itself by means of a Coanda jet that exhausts along the IGV's trailing edge surface. The IGV is …

    vt Repository record for 2D CFD Simulation of a Circulation Control Inlet Guide Vane (opens in a new tab)

  6. Heat transfer modeling of jet vane Thrust Vector Control (TVC) Systems

    … presented herein, analyzes two models of a jetvane Thrust Vector Control (TVC) System. Computational modeling was accomplished using the latest version of the PHOENICS computer code, designated PHOENICS-84. The vane configurations studied, consisted of a simple wedge and a blunt bodied vane, …

    nps Repository record for Heat transfer modeling of jet vane Thrust Vector Control (TVC) Systems (opens in a new tab)

  7. A Method to Characterize Gas Turbine Vane Performance Using Infrared Thermography

    Gas turbine vanes find themselves in very hostile environments – extremely high temperature combustion gases, much exceeding material melting temperatures, flowing over them at enormous pressures. It is necessitated due to the increased efficiency and power output at these conditions. However, this …

    vt Repository record for A Method to Characterize Gas Turbine Vane Performance Using Infrared Thermography (opens in a new tab)

  8. Effects of Realistic Combustor Exit Profiles on a Turbine Vane Endwall

    … and flow field non-uniformities, make turbine vane and endwall cooling a very critical issue in engine design. To appropriately cool these surfaces, knowledge of the passage flow field and endwall temperature distribution at representative engine conditions is necessary. A combustor test …

    vt Repository record for Effects of Realistic Combustor Exit Profiles on a Turbine Vane Endwall (opens in a new tab)

  9. Measurements and Predictions of Heat Transfer for a First Vane Design

    … on the heat transfer of a scaled-up stator vane. Understanding the three-dimensional effects of contoured endwalls on vane heat transfer can lead to prolonging blade life. The results of a combined experimental and computational study of heat transfer along the surface of a turbine vane that …

    vt Repository record for Measurements and Predictions of Heat Transfer for a First Vane Design (opens in a new tab)

  10. Noise due to pressure pulsations in a pressure-balanced sliding vane pump

    … of noise in a pressure-balanced sliding vane pump was conducted. The test pump for this research was used in an automobile's hydraulic power steering system. As currently designed, a small portion of the manufactured pumps generate excessive noise during operation. An experimental test …

    vt Repository record for Noise due to pressure pulsations in a pressure-balanced sliding vane pump (opens in a new tab)

  11. Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane

    An aerodynamic investigation was performed to assess the effectiveness of combined boundary layer suction and trailing edge blowing at reducing the blade profile losses and the wake momentum deficit of a cascade of tandem IGV's operating at realistic flow conditions. Two trailing edge blowing …

    vt Repository record for Effects of Flow Control on the Aerodynamics of a Tandem Inlet Guide Vane (opens in a new tab)

  12. Syngas ash deposition for a three row film cooled leading edge turbine vane

    … the dynamics of ash deposition in a leading edge vane geometry with film cooling. Large Eddy Simulations (LES) is used to model the flow field of the coolant jet-mainstream interaction and the deposition of syngas ash in the leading edge region of a turbine vane is modeled using a Lagrangian …

    vt Repository record for Syngas ash deposition for a three row film cooled leading edge turbine vane (opens in a new tab)

  13. Analysis of a Coupled Micro- and Triple-Impingement Cooling Configuration in the C3X Vane

    … the trailing edge protection of a turbine vane by incorporating two concepts from the literature. These two concepts are optimized near wall cooling passages and a triple-impingement configuration in the vane trailing edge. Finally this study explores a CFD conjugate analysis based on the …

    embry-riddle Repository record for Analysis of a Coupled Micro- and Triple-Impingement Cooling Configuration in the C3X Vane (opens in a new tab)

  14. Using Motor Electrical Signature Analysis to Determine the Mechanical Condition of Vane-Axial Fans

    … faults and fan imbalances could be detected in vane-axial fans using Motor Electrical Signature Analysis (MESA). The data was statistically analyzed to determine if the MESA systems could distinguish between baseline conditions and discrete fault frequencies for the three test conditions: …

    unt Repository record for Using Motor Electrical Signature Analysis to Determine the Mechanical Condition of Vane-Axial Fans (opens in a new tab)

  15. Single-Phase Heat Transfer Effects of Mixing Vane Geometries in a Narrow Rectangular Channel

    Mixing vane geometries enhance the fuel-to-coolant heat transfer within nuclear reactors, which allows for more efficient use of power reactors. At the same time, their presence affects the critical heat flux (CHF), the upper limit to power produced by the reactor, within the reactor. Numerical …

    mit Repository record for Single-Phase Heat Transfer Effects of Mixing Vane Geometries in a Narrow Rectangular Channel (opens in a new tab)

  16. Effects of Inlet Guide Vane Flow Control on Forced Response of a Transonic Fan

    … by an upstream row of stators or inlet guide vanes. Resonant response to engine order excitation at certain rotor speeds is especially damaging. Studies have shown that flow control by trailing edge blowing (TEB) can reduce stator wake strength and the amplitude of the downstream rotor blade …

    vt Repository record for Effects of Inlet Guide Vane Flow Control on Forced Response of a Transonic Fan (opens in a new tab)

  17. A Lean-Premixed Hydrogen Injector with Vane Driven Swirl for Application in Gas Turbines

    Hydrogen, as an alternative to conventional aviation fuels, has the potential to increase the efficiency of a gas turbine as well as reduce emissions of greenhouse gases. In addition to significantly reducing the number of pollutants due to the absence of carbon, burning hydrogen at low equivalence …

    vt Repository record for A Lean-Premixed Hydrogen Injector with Vane Driven Swirl for Application in Gas Turbines (opens in a new tab)

  18. Predictions and Measurements of Film-Cooling on the Endwall of a First Stage Vane

    … is the endwall of the first stage nozzle guide vane. This thesis details the design, prediction, and testing of two endwall film-cooling hole patterns provided by leading gas turbine engine companies. In addition a flush, two-dimensional slot was included to simulate leakage flow from the …

    vt Repository record for Predictions and Measurements of Film-Cooling on the Endwall of a First Stage Vane (opens in a new tab)

  19. Heat Transfer Coefficient and Adiabatic Effectiveness Measurements for an Internal Turbine Vane Cooling Feature

    Aircraft engine manufacturers strive for greater performance and efficiency by continually increasing the turbine inlet temperature. High turbine inlet temperatures significantly degrade the lifetime of components in the turbine. Modern gas turbines operate with turbine inlet temperatures well …

    vt Repository record for Heat Transfer Coefficient and Adiabatic Effectiveness Measurements for an Internal Turbine Vane Cooling Feature (opens in a new tab)

  20. Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade

    … on turbines performance through the nozzle guide vane passages. The current experimental aerodynamic investigation over the nozzle guide vane passage was concentrated on the backward-facing step of upstream misalignments. The tests were performed using two types of vane endwall platforms in a 2D …

    vt Repository record for Aerodynamic Investigation of Upstream Misalignment over the Nozzle Guide Vane in a Transonic Cascade (opens in a new tab)

Page 1 of 11