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Showing 1 to 20 of 509 for “"Gas turbine"”.

  1. Modelling Gas Turbine Degradation

    … of hot corrosion and related phenomenon in gas turbines using Reynolds-averaged Navier Stokes (RANS) computational fluid dynamics (CFD) simulations. Non-uniform distribution of gaseous species as a result of film coolant injection was observed on a simple single hole test case. RANS …

    cambridge Repository record for Modelling Gas Turbine Degradation (opens in a new tab)

  2. Gas turbine blade cooling

    Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Mechanical Engineering, 1947.

    mit Repository record for Gas turbine blade cooling (opens in a new tab)

  3. Humidification Processes in Gas Turbine Cycles

    … climate change caused by emissions of greenhouse gases from combustion processes has been recognized as a continuously growing problem and much research focuses on improving the environmental performance of gas turbines. The potential of improving gas turbine component efficiencies has become …

    lund Repository record for Humidification Processes in Gas Turbine Cycles (opens in a new tab)

  4. THE ECONOMICS OF GAS TURBINE COGENERATION.

    … economic viability of cogeneration. Employing a gas turbine system as a representative installation, the variables used in the sensitivity study are presented along with the justification for the assignment of the baseline and study range values. A simplified method for analyzing the …

    arizona-thes Repository record for THE ECONOMICS OF GAS TURBINE COGENERATION. (opens in a new tab)

  5. Blow-off in gas turbine combustors

    … with those obtained for the non-premixed gaseous case form a wide body of experimental data available for the validation of turbulent flame models. The quantification of some properties during the blow-off transient can assist studies of extinction based on large-eddy simulation that have …

    cambridge

  6. Design of a marine gas turbine

    Thesis (M.S.) Massachusetts Institute of Technology. Dept. of Naval Architecture and Marine Engineering, 1946.

    mit Repository record for Design of a marine gas turbine (opens in a new tab)

  7. Performance analysis of gas turbine cogeneration systems.

    … In the present work, performance of two gas turbine cogeneration systems is analyzed using the first and second laws of thermodynamics. A basic gas turbine cogeneration system and a steam injection gas turbine cogeneration system are investigated. In the analysis the system components, …

    uoit Repository record for Performance analysis of gas turbine cogeneration systems. (opens in a new tab)

  8. 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)

  9. Primary zone modeling for gas turbine combustors

    Gas turbine combustor primary zone flows are typified by swirling flow with heat release in a variable area duct, where a central toroidal recirculation zone is formed. The goal of the research was to develop reduced-order models for these flows in an attempt to gain insight into, and understanding …

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

  10. Study of a Nernst type gas turbine

    Thesis: B.S., Massachusetts Institute of Technology, Department of Chemical Engineering, 1953

    mit Repository record for Study of a Nernst type gas turbine (opens in a new tab)

  11. Probabilistic aerothermal design of gas turbine combustors

    … and the variability of the near-wall combustor gas temperature, respectively.

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

  12. Modeling and Control of Gas Turbine Thermoacoustic Pulsations

    … der Analyse thermoakustischer Instabilitäten in Gasturbinen-Brennkammern. Passive Methoden wurden entwickelt, um die durch die Instabilitäten entstehenden Druckschwankungen zu unterdrücken. Zunächst wurden unter der Annahme kleiner Mach-Zahlen die thermoakustischen Gleichungen hergeleitet. Die …

    tu-berlin Repository record for Modeling and Control of Gas Turbine Thermoacoustic Pulsations (opens in a new tab)

  13. GAS TURBINE CONVERSION FROM LIQUID TO GASEOUS FUEL

    … combustion engines to operate with renewable gaseous fuels, namely hydrogen gas. To test this hypothesis, performance measurements and internal inspection were conducted on the JetCat P60-SE turbojet, a small commercial gas turbine engine designed for remote-controlled hobby jets. The results …

    nps Repository record for GAS TURBINE CONVERSION FROM LIQUID TO GASEOUS FUEL (opens in a new tab)

  14. Linear and Nonlinear Modelling of Gas Turbine Engines

    … flow and shaft speeds of a Rolls Royce aircraft gas turbine. It is motivated by the desire to exploit recent advances in modelling linear and nonlinear systems and the need to investigate the suitability of various model representations in nonlinear gas turbine modelling.<br/><br/>The first part …

    southwales Repository record for Linear and Nonlinear Modelling of Gas Turbine Engines (opens in a new tab)

  15. 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)

  16. Commercial gas turbine engine platform strategy and design

    … the Pratt & Whitney PW4000 family of commercial gas turbine engines where predicted platform elements were consistent with actual design choices.

    mit Repository record for Commercial gas turbine engine platform strategy and design (opens in a new tab)

  17. Design of an automobile turbocharger gas turbine engine

    The turbocharger gas turbine engine was designed with the intent of being built as a demonstration for the Massachusetts Institute of Technology Department of Mechanical Engineering courses 2.005 and 2.006 to supplement material covered. A gas turbine operates on an open version of the Brayton …

    mit Repository record for Design of an automobile turbocharger gas turbine engine (opens in a new tab)

  18. Thermal design of a cooled micro gas turbine

    … challenges associated with designing a micro gas turbine engine is the problem of heat transfer. The demonstration version of the engine deals with this problem by transferring excess heat from the turbine, to the compressor wall, through the rotor shaft. This is necessary to keep the turbine

    mit Repository record for Thermal design of a cooled micro gas turbine (opens in a new tab)

  19. Materials substitution in aircraft gas turbine engine applications

    Thesis (Ph. D.)--Massachusetts Institute of Technology, Dept. of Materials Science and Engineering, 1992.

    mit Repository record for Materials substitution in aircraft gas turbine engine applications (opens in a new tab)

  20. Combustion gas generator for gas turbine exhaust systems modeling.

    A combustion gas generator was constructed for the purpose of modeling shipboard gas turbine engine exhaust systems. In particular, the system was designed and validated for exhaust stack Mach numbers in the neighborhood of 0.07 and exhaust stack temperatures varying from 700 to 900°F with an …

    nps Repository record for Combustion gas generator for gas turbine exhaust systems modeling. (opens in a new tab)

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