Flame Temperature Estimation of Conventional and Future Jet FuelsSource: Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002::page 376Author:Ö. L. Gülder
DOI: 10.1115/1.3239914Publisher: The American Society of Mechanical Engineers (ASME)
Abstract: An approximate formula is presented by means of which the adiabatic flame temperature of jet fuel-air systems can be calculated as functions of pressure, temperature, equivalence ratio, and hydrogen to carbon atomic ratio of the fuel. The formula has been developed by fitting of the data from a detailed chemical equilibrium code to a functional expression. Comparisons of the results from the proposed formula with the results obtained from a chemical equilibrium code have shown that the average error in estimated temperatures is around 0.4 percent, the maximum error being less than 0.8 percent. This formula provides a very fast and easy means of predicting flame temperatures as compared to thermodynamic equilibrium calculations, and it is also applicable to diesel fuels, gasolines, pure alkanes, and aromatics as well as jet fuels.
keyword(s): Jet fuels , Temperature , Flames , Formulas , Fuels , Equilibrium (Physics) , Errors , Fittings , Carbon , Diesel , Functions , Hydrogen AND Pressure ,
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| contributor author | Ö. L. Gülder | |
| date accessioned | 2017-05-08T23:22:29Z | |
| date available | 2017-05-08T23:22:29Z | |
| date copyright | April, 1986 | |
| date issued | 1986 | |
| identifier issn | 1528-8919 | |
| identifier other | JETPEZ-26634#376_1.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/101138 | |
| description abstract | An approximate formula is presented by means of which the adiabatic flame temperature of jet fuel-air systems can be calculated as functions of pressure, temperature, equivalence ratio, and hydrogen to carbon atomic ratio of the fuel. The formula has been developed by fitting of the data from a detailed chemical equilibrium code to a functional expression. Comparisons of the results from the proposed formula with the results obtained from a chemical equilibrium code have shown that the average error in estimated temperatures is around 0.4 percent, the maximum error being less than 0.8 percent. This formula provides a very fast and easy means of predicting flame temperatures as compared to thermodynamic equilibrium calculations, and it is also applicable to diesel fuels, gasolines, pure alkanes, and aromatics as well as jet fuels. | |
| publisher | The American Society of Mechanical Engineers (ASME) | |
| title | Flame Temperature Estimation of Conventional and Future Jet Fuels | |
| type | Journal Paper | |
| journal volume | 108 | |
| journal issue | 2 | |
| journal title | Journal of Engineering for Gas Turbines and Power | |
| identifier doi | 10.1115/1.3239914 | |
| journal fristpage | 376 | |
| journal lastpage | 380 | |
| identifier eissn | 0742-4795 | |
| keywords | Jet fuels | |
| keywords | Temperature | |
| keywords | Flames | |
| keywords | Formulas | |
| keywords | Fuels | |
| keywords | Equilibrium (Physics) | |
| keywords | Errors | |
| keywords | Fittings | |
| keywords | Carbon | |
| keywords | Diesel | |
| keywords | Functions | |
| keywords | Hydrogen AND Pressure | |
| tree | Journal of Engineering for Gas Turbines and Power:;1986:;volume( 108 ):;issue: 002 | |
| contenttype | Fulltext |