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Showing 1 to 19 of 19 for “"Gas turbine combustion"”.

  1. Impact of alternative jet fuels on gas turbine combustion systems

    … what fuel properties rate-limit the combustion process across a variety of engine-relevant operating conditions can dramatically shorten fuel certification times and decrease testing costs. The central objective of this work is to determine which fuel properties govern whether …

    uiuc Repository record for Impact of alternative jet fuels on gas turbine combustion systems (opens in a new tab)

  2. Modeling Hydrodynamic Stability of Incline-Liquid Airblast Nozzle for Gas Turbine Combustion

    … fuel and air is a critical process for optimum combustion in gas turbine engines due to its high influence on the downstream combustion process. The need for minimizing fuel consumption coupled with the requirement for combustion systems to perform well at all flight conditions puts the …

    embry-riddle Repository record for Modeling Hydrodynamic Stability of Incline-Liquid Airblast Nozzle for Gas Turbine Combustion (opens in a new tab)

  3. Study of alternative jet fuel ignition behavior in gas turbine combustion environments

    Submission published under a 24 month embargo labeled 'U of I Access', the embargo will last until 2025-05-01

    uiuc Repository record for Study of alternative jet fuel ignition behavior in gas turbine combustion environments (opens in a new tab)

  4. Thermal design and analysis of a recuperative combustor for gas-turbine combustion

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1993.

    mit Repository record for Thermal design and analysis of a recuperative combustor for gas-turbine combustion (opens in a new tab)

  5. Investigation of alternative jet fuels in gas turbine combustion systems using x-ray radiography

    … affect the atomization, vaporization, and combustion process of jet fuels and ascertain which properties determine if an alternative fuel will behave similarly to conventional jet fuel. In this work, x-ray phase-contrast imaging is performed at 90,517 Hz on a combusting fuel spray in a …

    uiuc Repository record for Investigation of alternative jet fuels in gas turbine combustion systems using x-ray radiography (opens in a new tab)

  6. A Thermoacoustic Characterization of a Rijke-type Tube Combustor

    … community, can cause extensive damage in gas turbine combustion chambers. To understand the phenomena related to thermoacoustics, a simple Rijke-type tube combustor was built and studied. Extensive experimental results, as well as theoretical analyses related to the Rijke tube are …

    vt Repository record for A Thermoacoustic Characterization of a Rijke-type Tube Combustor (opens in a new tab)

  7. An investigation into the origin, measurement and application of chemiluminescent light emissions from premixed flames

    … CH* and OH* are studied in premixed methane combustion to investigate the possible application of their light emissions in gas turbine combustion monitoring systems. The interpretation of integrated and local chemiluminescence measurements are shown to give important qualitative insights into …

    vt Repository record for An investigation into the origin, measurement and application of chemiluminescent light emissions from premixed flames (opens in a new tab)

  8. Nonlinear Control of a Thermoacoustic System with Multiple Heat Sources and Actuators

    … lead to unpredictable behavior of the system. Gas-turbine combustion systems are especially prone to this phenomenon reducing their overall efficiency. Additionally, due to the nature of the combustion, the turbines end up releasing undesired amounts of harmful chemicals to the atmosphere, such …

    embry-riddle Repository record for Nonlinear Control of a Thermoacoustic System with Multiple Heat Sources and Actuators (opens in a new tab)

  9. Combustion Instability Mechanism of a Reacting Jet in Cross Flow at Gas Turbine Operating Conditions

    Modern gas turbine designs often include lean premixed combustion for its emissions benefits; however, this type of combustion process is susceptible to self-excited combustion instabilities that can lead to damaging heat loads and system vibrations. This study focuses on identifying a mechanism of …

    ucf

  10. A method for the numerical analysis of combustion instabilities with an application to afterburner screech

    … damaging thermoacoustic oscillations in gas turbine combustion systems by computational means. A framework is laid out to predict numerically the frequency and stability of thermoacoustic oscillations, with focus on the high frequency screech instability of afterburners. A hybrid …

    cambridge Repository record for A method for the numerical analysis of combustion instabilities with an application to afterburner screech (opens in a new tab)

  11. Global stability and control of swirling jets and flames

    … of many practical flows, such as those found in gas turbine combustion chambers. This thesis is concerned primarily with large-scale unsteady structures that arise due to self-sustained hydrodynamic oscillations, also known as global hydrodynamic instability. Direct numerical simulation (DNS) of …

    cambridge Repository record for Global stability and control of swirling jets and flames (opens in a new tab)

  12. Large eddy simulation of primary liquid-sheet breakup

    … capability to simulate the fuel injection in gas turbine combustion chambers. The path to this objective started with the review of state-of-the-art numerical techniques to model the primary breakup of liquid fuel into droplets. Based on this and keeping in mind the requirements of the …

    cambridge Repository record for Large eddy simulation of primary liquid-sheet breakup (opens in a new tab)

  13. Investigation of a prototype industrial gas turbine combustor using alternative gaseous fuels

    In this thesis, the effect of alternative gaseous fuels, with high hydrogen content and lower calorific value, on gas turbine combustion was investigated experimentally. The aim of the investigation was to find operational limitations for an experimental burner and to supply data for validation of …

    lund Repository record for Investigation of a prototype industrial gas turbine combustor using alternative gaseous fuels (opens in a new tab)

  14. Study of Lean Blowout Limits and Effects of Near Blowout Oscillations on Flow Field and Heat Transfer on Gas Turbine Combustor

    Modern gas turbine combustors implement lean premixed (LPM) combustion system to reduce the formation of NOx pollutants. LPM technology has advanced to have the ability to produce extremely low level of NOx emissions. The current focus of research on LPM is focused on reducing the NOx emission to …

    vt Repository record for Study of Lean Blowout Limits and Effects of Near Blowout Oscillations on Flow Field and Heat Transfer on Gas Turbine Combustor (opens in a new tab)

  15. Spatially Resolved Analysis of Flame Dynamics for the Prediction of Thermoacoustic Combustion Instabilities

    … stringent emissions regulations have led combustion system designers to look for more environmentally combustion strategies. For gas turbine combustion, one promising technology is lean premixed combustion, which results in lower flame temperatures and therefore the possibility of …

    vt Repository record for Spatially Resolved Analysis of Flame Dynamics for the Prediction of Thermoacoustic Combustion Instabilities (opens in a new tab)

  16. Characterization of compact gas turbine combustors for alternative fuel integration

    The student, Eric Wood, submitted this Dissertation for approval on 2023-07-06 at 09:50.

    uiuc Repository record for Characterization of compact gas turbine combustors for alternative fuel integration (opens in a new tab)

  17. Thermoacoustic Analysis and Experimental Validation of Statistically-Based Flame Transfer Function Extracted from Computational Fluid Dynamics

    … with the Flamelet Generated Manifold (FGM) combustion model are performed and probability density functions (PDFs) of the convective time delay and local heat release rates are extracted. These are then used as inputs to the 1-D Thermoacoustic model. Results are compared with the …

    vt Repository record for Thermoacoustic Analysis and Experimental Validation of Statistically-Based Flame Transfer Function Extracted from Computational Fluid Dynamics (opens in a new tab)

  18. Laser Induced Incandescence for Volume Fraction and Relative Particle Size Measurements in a Rich-Quench-Lean Jet A Combustor

    Reducing the production of nonvolatile particulate matter, which is composed mostly of soot, is an important goal for modern aeroengine combustors. Not only does soot production reduce engine performance, but it also creates unwanted pollution. In order to understand soot production in realistic …

    gatech Repository record for Laser Induced Incandescence for Volume Fraction and Relative Particle Size Measurements in a Rich-Quench-Lean Jet A Combustor (opens in a new tab)