The Influence of Fuel Variables on Radiation From Flames in a Turbojet Combustor

Randall, N. P.; Ritcheske, W. F.

doi:10.4271/590405

Cited by 4 publications

(2 citation statements)

References 1 publication

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“…Equation (29) specifies the value of flame luminosity as used for the current work. It was derived from data from several sources (11)(12)(13)(14)(15)(16)1) and represents the best-fit line to the data available. It has proved satisfactory for most applications to date, but it has obvious limitations.…”

Section: Determination Of the Flame Luminosity And Emissivitymentioning

confidence: 99%

A Simple Method for the Prediction of Wall Temperatures in Gas Turbines

Kretschmer

Odgers

1978

Volume 1A: General

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The cited method predicts wall temperatures generally within an accuracy of f 6 percent. The biggest single factor governing the wall temperature is shown to be the hot gas temperature. Other factors discussed are the effects of changes in inlet temperature, fuel types, the geometry of the film cooling devices and manufacturing tolerances. Empirical formulas are given for the prediction of effective temperatures within the various combustor zones. Some comparisons are made between predictions and measurements of wall temperatures over a range of operating conditions.

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Section: Determination Of the Flame Luminosity And Emissivitymentioning

confidence: 99%

A Simple Method for the Prediction of Wall Temperatures in Gas Turbines

Kretschmer

Odgers

1978

Volume 1A: General

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“…Equation (29) specifies the value of flame luminosity as used for the current work. It was derived from data from several sources [1,[10][11][12][13][14][15] and represents the best-fit line to the data available. It has proved satisfactory for most applications to date, but it has obvious limitations.…”

Section: Determination Of the Flame Luminosity And Emissivitymentioning

confidence: 99%

Erratum: “A Simple Method for the Prediction of Wall Temperatures in Gas Turbines” [ASME 1978 International Gas Turbine Conference and Products Show, Volume 1A: General, London, England, April 9–13, 1978, Conference Sponsors: International Gas Turbine Institute, ISBN: 978-0-7918-7971-9, Copyright © 1978 by ASME. Paper No. 78-GT-90, V01AT01A090; 13 pages; doi: 10.1115/78-GT-90]

Kretschmer

Odgers

1978

Volume 1A: General

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This erratum corrects errors that appeared in the paper “A Simple Method for the Prediction of Wall Temperatures in Gas Turbines”, which was published in Proceedings of the ASME 1978 International Gas Turbine Conference and Products Show, Volume 1A: General, V01AT01A090, April 1978, 78-GT-90, doi: 10.1115/78-GT-90. This paper was originally published in 1978. There were numerous equation errors due to the typesetting limitations which have been corrected. The references have also been updated to contain additional information. Reference 12 is a duplicate of reference 10 and has also been removed.

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Progress and problems in gas-turbine combustion

Lefebvre

1965

Symposium (International) on Combustion

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The Influence of Fuel Variables on Radiation From Flames in a Turbojet Combustor

Cited by 4 publications

References 1 publication

A Simple Method for the Prediction of Wall Temperatures in Gas Turbines

A Simple Method for the Prediction of Wall Temperatures in Gas Turbines

Progress and problems in gas-turbine combustion

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