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Showing 1 to 20 of 133 for “"Combustors"”.

  1. Transient Phenomena in Annular Combustors

    … related to the operation of annular gas turbine combustors, namely ignition and blow-off. The experiments were conducted on complex multi-burner geometries, close to realistic combustors, to provide a wide data set including stability limits, flame regimes and physical mechanisms of ignition and …

    cambridge Repository record for Transient Phenomena in Annular Combustors (opens in a new tab)

  2. Simulations of turbulent swirl combustors

    … thesis aims at improving our knowledge on swirl combustors. The work presented here is based on Large Eddy Simulations (LES) coupled to an advanced combustion model: the Conditional Moment Closure (CMC). Numerical predictions have been systematically compared and validated with detailed …

    cambridge Repository record for Simulations of turbulent swirl combustors (opens in a new tab)

  3. Blow-off in gas turbine combustors

    This thesis describes an experimental investigation of the flame structure close to the extinction and the blow-off events of non-premixed and spray flames stabilized on an axisymmetric bluff body in a confined swirl configuration. The comparison of flames of different canonical types in the same …

    cambridge

  4. Dynamics of Lean Direct Injection Combustors

    Improvements to heritage gas turbine engines will be needed in the coming years as the demand made on these systems increase. While industry continually presses for higher performance of both military and civilian aero engines, the government simultaneously raises the bar for emissions standards in …

    vt Repository record for Dynamics of Lean Direct Injection Combustors (opens in a new tab)

  5. Fuel-flexible Gas Turbine Combustors for Decarbonization

    L'abstract è presente nell'allegato / the abstract is in the attachment

    poli-torino Repository record for Fuel-flexible Gas Turbine Combustors for Decarbonization (opens in a new tab)

  6. Primary zone modeling for gas turbine combustors

    … addition at conditions typical of gas turbine combustors, (ii) to assess the relative merits of various reduced-order models, and (iii) to define the applicability of these models in the design process. To this end, several reduced-order models of combustor primary zones were developed and …

    mit Repository record for Primary zone modeling for gas turbine combustors (opens in a new tab)

  7. Probabilistic aerothermal design of gas turbine combustors

    … estimated using deterministic methods for these combustors, and the probability that a randomly selected combustor will fail earlier than predicted using deterministic methods is approximately 80 percent. Finally, the application of a sensitivity analysis to a surrogate model for the life …

    mit Repository record for Probabilistic aerothermal design of gas turbine combustors (opens in a new tab)

  8. Turbulent combustion simulation in realistic gas-turbine combustors

    The work presented in this thesis addresses issues involving the accurate and efficient numerical modelling of turbulence combustion with an emphasis on an industrially representative Tay model combustor. This combustor retained all essential features of a modern aero-engine rich burn combustor and …

    city-london Repository record for Turbulent combustion simulation in realistic gas-turbine combustors (opens in a new tab)

  9. An Experimental Study of Transient Flows in Pulse Combustors

    <p>The purpose of this investigation was to experimentally characterize a pulse combustor with respect to ambient conditions, pressure amplitudes, wall temperature, combustor geometry and type of centerbody used. The wall temperatures were recorded and the pressure variation was obtained using a …

    embry-riddle Repository record for An Experimental Study of Transient Flows in Pulse Combustors (opens in a new tab)

  10. Numerical investigation of the instability of premixed dump combustors

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1989.

    mit Repository record for Numerical investigation of the instability of premixed dump combustors (opens in a new tab)

  11. One-Dimensional, Finite-Rate Model for Gas-Turbine Combustors

    … been developed for the analysis for gas-turbine combustors. The basis of the model is the one-dimensional, integral form of the conservation equations for multi-species, non-equilibrium, reacting mixtures. Special procedures were devised for the flow-division of the inlet flow into primary- and …

    vt Repository record for One-Dimensional, Finite-Rate Model for Gas-Turbine Combustors (opens in a new tab)

  12. Acoustic performance of bias flow liners in gas turbine combustors

    Der Einsatz moderner Verbrennungskonzepte zur Effizienzsteigerung und Schadstoffreduktion bei Gasturbinen wird oft durch thermo-akustische Instabilitäten verhindert. Durchströmte Brennkammerliner können die akustische Dämpfung des Systems erhöhen und die Instabilitäten unterdrücken. Eine …

    tu-berlin Repository record for Acoustic performance of bias flow liners in gas turbine combustors (opens in a new tab)

  13. 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)

  14. Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors

    … on predicting this behaviour in annular combustors. The complexity of the annular design can give rise to an additional set of intricate oscillations due to the presence of interactions between neighbouring flames. The project is concerned with capturing trends in oscillatory behaviour in …

    cambridge Repository record for Computational Fluid Dynamics Investigation of Oscillatory Behaviour in Annular Combustors (opens in a new tab)

  15. A physics-based emissions model for aircraft gas turbine combustors

    … and CO emissions from five different industry combustors to certification data. The model developed in this work correctly captures the physical relationships between engine operating conditions, combustor design parameters, and NO. and CO emissions. The NO. estimates are as good as, or better …

    mit Repository record for A physics-based emissions model for aircraft gas turbine combustors (opens in a new tab)

  16. Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors

    A flush-wall injector model and a strut injector model representative of state of the art scramjet engine combustion chambers were experimentally studied in a cold-flow (non-combusting) environment to determine their fuel-air mixing behavior under different operating conditions. The experiments …

    vt Repository record for Experimental Studies of Injector Array Configurations for Circular Scramjet Combustors (opens in a new tab)

  17. Effect of inlet configurations on the aerodynamics of swirl combustors

    The flowfield in a swirling combustor with a Confinement Ratio of 1.6 was simulated in water. Qualitative measurements were made from flow visualization in a horizontal water rig with the help of Pliolite beads and liquid dye. Velocity and turbulence measurements were made in a cold air flow rig. …

    vt Repository record for Effect of inlet configurations on the aerodynamics of swirl combustors (opens in a new tab)

  18. Fuel Droplet Optical Diagnostic Techniques for Lean Premixed Prevaporized Aeroengine Combustors

    … the performance and limitations of these combustors. Thus, a key focus is the analysis of fuel droplets in these combustors across various CST relevant operating conditions. This work employs a combination of optical diagnostics to enhance the understanding of fuel spray dynamics. Here, …

    gatech Repository record for Fuel Droplet Optical Diagnostic Techniques for Lean Premixed Prevaporized Aeroengine Combustors (opens in a new tab)

  19. Hydrodynamic scaling and solids mixing in pressurized bubbling fluidized bed combustors

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1996.

    mit Repository record for Hydrodynamic scaling and solids mixing in pressurized bubbling fluidized bed combustors (opens in a new tab)

  20. Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors

    <p>The goal of this study is to establish the dominant flow structure required to effectively accelerate the turbulent deflagration flame front to detonation velocity in the shortest possible distance while using a single Jet in Cross Flow (JICF). Jets in crossflow, depending on orientation and …

    embry-riddle Repository record for Fluidic Jet Turbulence Generators for Deflagration to Detonation Transition in Pulsed Detonation Combustors (opens in a new tab)

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