December 4, 2020

Download Ebook Free Determination Of Primary Zone Smoke Concentrations From Spectral Radiance Measurements In Gas Turbine Combustors

Determination of Primary-zone Smoke Concentrations from Spectral Radiance Measurements in Gas Turbine Combustors

Determination of Primary-zone Smoke Concentrations from Spectral Radiance Measurements in Gas Turbine Combustors
Author : Carl T. Norgren
Publisher : Unknown
Release Date : 1971
Category : Combustion chambers
Total pages :46
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The smoke concentration within the primary zone of an experimental combustor operating at pressures up to 20 atmospheres was determined with a technique using spectral radiance measurements. Exhaust smoke concentration was obtained from reflectance readings of stained filter paper. The primary zone smoke concentration was of the order of 100 to 1000 times greater than at the exhaust. The smoke oxidation rate obtained is compared with reported values for coal particles and seeded laboratory flames. Primary zone smoke concentration was shown to be related to exhaust smoke number and total radiance.

NASA Technical Note

NASA Technical Note
Author : United States. National Aeronautics and Space Administration
Publisher : Unknown
Release Date : 1971
Category : Aeronautics
Total pages :129
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NASA technical note

NASA technical note
Author : Anonim
Publisher : Unknown
Release Date : 1971
Category : Aeronautics
Total pages :129
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Emissions from Continuous Combustion Systems

Emissions from Continuous Combustion Systems
Author : W. Cornelius
Publisher : Springer Science & Business Media
Release Date : 2013-03-09
Category : Science
Total pages :479
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This volume documents the proceedings of the Symposium on Emissions from Continuous Combustion Systems that was held at the General Motors Research Laboratories, Warren, Michigan on September 27 and 28, 1971. This symposium was the fifteenth in an annual series presented by the Research Laboratories. Each symposium has covered a different technical discipline. To be selected as the theme of a symposium, the subject must be timely and of vital interest to General Motors as well as to the technical community at large. For each symposium, the practice is to solicit papers at the forefront of research from recognized authorities in the technical discipline of interest. Approximately sixty scientists and engineers from academic, government and industrial circles in this country and abroad are then invited to join about an equal number of General Motors technical personnel to discuss freely the commissioned papers. The technical portion of the meeting is supplemented by social functions at which ample time is afforded for informal exchanges of ideas amongst the participants. By such a direct interaction of a small and select group of informed participants, it is hoped to extend the boundaries of research in the selected technical field.

Scientific and Technical Aerospace Reports

Scientific and Technical Aerospace Reports
Author : Anonim
Publisher : Unknown
Release Date : 1971
Category : Aeronautics
Total pages :129
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Spectral radiance measurements and calculated soot concentrations along the length of an experimental combustor

Spectral radiance measurements and calculated soot concentrations along the length of an experimental combustor
Author : Carl T. Norgren,Robert D. Ingebo
Publisher : Unknown
Release Date : 1976
Category : Airplanes
Total pages :23
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Turbine Technology

Turbine Technology
Author : Anonim
Publisher : Unknown
Release Date : 1971
Category : Automobiles, Gas-turbine
Total pages :129
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Spectral Flame Radiance from a Tubular-can Combustor

Spectral Flame Radiance from a Tubular-can Combustor
Author : Russell W. Claus
Publisher : Unknown
Release Date : 1981
Category : Flame spectroscopy
Total pages :13
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Spectral Flame Radiance from a Tubular-can Combustor

Spectral Flame Radiance from a Tubular-can Combustor
Author : Anonim
Publisher : Unknown
Release Date : 1981
Category :
Total pages :15
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Applied Mechanics Reviews

Applied Mechanics Reviews
Author : Anonim
Publisher : Unknown
Release Date : 1972
Category : Mechanics, Applied
Total pages :129
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Effects of Broadened Property Fuels on Radiant Heat Flux to Gas Turbine Combustor Liners

Effects of Broadened Property Fuels on Radiant Heat Flux to Gas Turbine Combustor Liners
Author : Anonim
Publisher : Unknown
Release Date : 1983
Category :
Total pages :27
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High-pressure Performance of Combustor Segments Utilizing Pressure-atomizing Fuel Nozzles and Air Swirlers for Primary-zone Mixing

High-pressure Performance of Combustor Segments Utilizing Pressure-atomizing Fuel Nozzles and Air Swirlers for Primary-zone Mixing
Author : Robert D. Ingebo,Albert J. Doskocil,Carl T. Norgren
Publisher : Unknown
Release Date : 1971
Category :
Total pages :36
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Spectral Structure of Pressure Measurements Made in a Combustion Duct

Spectral Structure of Pressure Measurements Made in a Combustion Duct
Author : J. H. Miles
Publisher : Unknown
Release Date : 1980
Category :
Total pages :46
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High-pressure Combustor Exhaust Emissions with Improved Air-atomizing and Conventional Pressure-atomizing Fuel Nozzles

High-pressure Combustor Exhaust Emissions with Improved Air-atomizing and Conventional Pressure-atomizing Fuel Nozzles
Author : Robert D. Ingebo,Carl T. Norgren
Publisher : Unknown
Release Date : 1973
Category : Aircraft exhaust emissions
Total pages :22
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A high-pressure combustor segment 0.456 meter (18 in.) long with a maximum cross section of 0.153 by 0.305 meter (6 by 12 in.) was tested with specially designed air-atomizing and conventional pressure-atomizing fuel nozzles at inlet-air temperatures of 340 to 755 k (610 deg to 1360 R), reference velocities of 12.4 to 26.1 meters per second (41 to 86 ft/sec), and fuel-air ratios of 0.008 to 0.020. Increasing inlet-air pressure from 4 to 20 atmospheres generally increased smoke number and nitric oxide, but decreased carbon monoxide and unburned hydrocarbon concentrations with air-atomizing and pressure-atomizing nozzles. Emission indexes for carbon monoxide and unburned hydrocarbons were lower at 4, 10, and 20 atmospheres, and nitric oxide emission indexes were lower at 10 and 20 atmospheres with air-atomizing than with pressure-atomizing nozzles.

Performance and emission characteristics of swirl-can combustors to a near-stoichiometric fuel-air ratio

Performance and emission characteristics of swirl-can combustors to a near-stoichiometric fuel-air ratio
Author : Larry A. Diehl,Arthur M. Trout
Publisher : Unknown
Release Date : 1976
Category : Air
Total pages :39
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