Subsonic Flow Flameholder Studies Using a Low Pressure Simulation Technique

Norster, E. R.

doi:10.1016/b978-0-08-013275-4.50010-6

Cited by 3 publications

(1 citation statement)

References 7 publications

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“…It requires pre-heating of the inlet air to ensure complete vaporization of the droplets. Gaseous nitrogen has also been used with success (Norster, 1968), and does not require pre-heating. Although a direct calibration for nitrogen was not available, nitrogen as a diluent is extremely convenient for the present purposes, and was therefore selected.…”

Section: Simulation Techniquementioning

confidence: 99%

Lean Blowout in a Research Combustor at Simulated Low Pressures

Sturgess

Heneghan

Vangsness

et al. 1991

Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations

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A propane-fueled research combustor has been designed to represent the essential features of primary zones of combustors for aircraft gas turbine engines in an investigation of lean blowouts. The atmospheric pressure test facility being used for the investigation made it difficult to directly approach the maximum heat release condition of the research combustor. High combustor loadings were achieved through simulating the effects on chemical reaction rates of sub-atmospheric pressures by means of a nitrogen diluent technique. A calibration procedure is described, and correlated experimental lean blowout results are compared with well-stirred reactor calculations for the research combustor to confirm the efficacy of the calibration.

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Section: Simulation Techniquementioning

confidence: 99%

Lean Blowout in a Research Combustor at Simulated Low Pressures

Sturgess

Heneghan

Vangsness

et al. 1991

Volume 3: Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations

View full text Add to dashboard Cite

show abstract

Lean Blowout in a Research Combustor at Simulated Low Pressures

Sturgess

Heneghan

Vangsness

et al. 1996

Journal of Engineering for Gas Turbines and Power

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A propane-fueled research combustor has been designed to represent the essential features of primary zones of combustors for aircraft gas turbine engines in an investigation of lean blowouts. The atmospheric pressure test facility being used for the investigation made it difficult to approach the maximum heat release condition of the research combustor directly. High combustor loadings were achieved through simulating the effects on chemical reaction rates of subatmospheric pressures by means of a nitrogen diluent technique. A calibration procedure is described, and correlated experimental lean blowout results are compared with well-stirred reactor calculations for the research combustor to confirm the efficacy of the calibration.

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Combustion Performance

2010

Gas Turbine Combustion

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Subsonic Flow Flameholder Studies Using a Low Pressure Simulation Technique

Cited by 3 publications

References 7 publications

Lean Blowout in a Research Combustor at Simulated Low Pressures

Lean Blowout in a Research Combustor at Simulated Low Pressures

Lean Blowout in a Research Combustor at Simulated Low Pressures

Combustion Performance

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