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Showing 1 to 12 of 12 for “"Gas Generator"”.

  1. Surge dynamics of a helicopter engine gas generator

    Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.

    mit Repository record for Surge dynamics of a helicopter engine gas generator (opens in a new tab)

  2. 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)

  3. Visualization and velocity measurement of unsteady flow in a gas generator using cold-flow technique

    … cold flow techniques is discussed. The flow in a gas generator has been modeled using cold air. Experimental set up was designed and fabricated to simulate the unsteady flow with different configurations of inlet tubes. Tests were run for flow visualization and measurement of axial velocity at …

    vt Repository record for Visualization and velocity measurement of unsteady flow in a gas generator using cold-flow technique (opens in a new tab)

  4. Assessment of the Thermal Advantages of Biased Supersonic Cooling

    … film cooling method for hydrogen-fueled, gas-generator cycle rocket engines. The research is intended to serve as an initial proof-of-concept for a biased supersonic film cooling method envisioned for nozzle extension thermal management. The proposed method utilizes a dual-stream injection …

    embry-riddle Repository record for Assessment of the Thermal Advantages of Biased Supersonic Cooling (opens in a new tab)

  5. An Experimental Investigation into NOx Control of a Gas Turbine Combustor and Augmentor Tube Incorporating a Catalytic Reduction System

    … engine test cell environment. A modified T-63 gas turbine combustor and an augmentor tube, 21 feet in length and containing a perlite catalyst, were used as a gas generator and catalytic reduction system. Four data runs were made. Three runs were completed without the catalyst installed. …

    nps Repository record for An Experimental Investigation into NOx Control of a Gas Turbine Combustor and Augmentor Tube Incorporating a Catalytic Reduction System (opens in a new tab)

  6. Modeling and Optimization of Turbine-Based Combined-Cycle Engine Performance

    … impulse performance. The hydrocarbon-fueled gas-generator air turborocket and hydrogen-fueled expander-cycle air turborocket are also competitive because they may provide greater thrust-to-weight than the TBE, but require some engineering problems to be addressed before being fully developed.

    maryland Repository record for Modeling and Optimization of Turbine-Based Combined-Cycle Engine Performance (opens in a new tab)

  7. Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation

    … confidence. In the ducted rocket a solid fuel gas generator is used to deliver a fuel-rich multi-phase mixture to the combustion chamber. When a valve is used to vary the fuel generator pressure, and thereby the delivered fuel flowrate, the engine is known as a Variable Flow Ducted Rocket …

    vt Repository record for Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation (opens in a new tab)

  8. Experimental investigation of the flow field in a missile launch tube

    … potential hot spots. The mixing of the fuel-rich gas generator effulent and the air in the launch tube was assessed by thermocouple measurements; warm water was used to simulate the exhaust while ambient water represented the air initially contained in the launch tube. The results have shown that …

    vt Repository record for Experimental investigation of the flow field in a missile launch tube (opens in a new tab)

  9. Design of a High Specific Power Electric Machine for Turboelectric Propulsion

    … propulsion for aviation, in which a gas generator core electrically drives motor-powered propulsors, are limited by the mass and losses of the electric components introduced into the drivetrain. These propulsion systems are predicted to result in a 15\% fuel savings provided that …

    mit Repository record for Design of a High Specific Power Electric Machine for Turboelectric Propulsion (opens in a new tab)

  10. Failure detection, isolation and mitigation for a spacecraft solid fuel reaction control system

    … which commonly functions by burning a solid fuel gas generator and expelling gas out of valves arranged around the vehicle. Valve failures are known to occur in spacecraft reaction control systems, and without on-board, real time failure identification and mitigation, the Mars Ascent Vehicle could …

    mit Repository record for Failure detection, isolation and mitigation for a spacecraft solid fuel reaction control system (opens in a new tab)

  11. Investigation of thermally induced stresses in a transition-piece in relation to an aero-derivative gas turbine engine operation

    The transition-piece of an aero-derivative gas turbine engine transfers high temperature combusted gases from the gas generator to a power turbine, and it is manufactured from Iron-Base Superalloy A286 in this investigation. Due to the thermal stress levels developed in the casing of the …

    dcu Repository record for Investigation of thermally induced stresses in a transition-piece in relation to an aero-derivative gas turbine engine operation (opens in a new tab)

  12. Optimisation of Co-Firing of High Moisture Biomass with Coal in a Bubbling Fluidised Bed Combustor

    … of enhancing the of coal fired fluidised bed hot gas generator (HGG) at the Cantley factory of British Sugar. It covers combustion of coal and biomass and their blends also called co-firing in a fluidised bed combustor. Particularly it focuses on the effect of introduction of moisture as part of …

    southwales Repository record for Optimisation of Co-Firing of High Moisture Biomass with Coal in a Bubbling Fluidised Bed Combustor (opens in a new tab)