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NACA-RM-E52H15

Pressure limits of flame propagation of pure hydrocarbon-air mixtures at reduced pressure

Organization:
NASA - National Aeronautics and Space Administration (NASA)
Year: 1952

Abstract: The flammability limits of 18 high-boiling hydrocarbons at reduced pressures were studied in a closed flame tube with hot-wire ignition. Characteristic two-lobe flammability-limit curves were exhibited by all the hydrocarbons studied. The minimum pressure limit was not affected by the molecular weight.
The rich limit, the lean limit, and the flammability range, when expressed as volume percent fuel, decreased as the number of carbon atoms increased. However, if the concentration of fuel is expressed as percent stoichiometric, the lean limit of the n-alkanes and n-alkenes attains a maximum value near a molecular weight of 75. Likewise the rich limit of the same two series attains a maximum near a molecular weight of 100. The flammability range, when expressed as volume percent fuel in the mixture, correlated with the molecular weight raised to the -0.70 power. The rich Limit correlated with the lean limit raised to the 0.56 power.
URI: https://yse.yabesh.ir/std/handle/yse/8842
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    NACA-RM-E52H15

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contributor authorNASA - National Aeronautics and Space Administration (NASA)
date accessioned2017-09-04T15:10:32Z
date available2017-09-04T15:10:32Z
date copyright01/01/1952
date issued1952
identifier otherLRONEEAAAAAAAAAA.pdf
identifier urihttps://yse.yabesh.ir/std/handle/yse/8842
description abstractThe flammability limits of 18 high-boiling hydrocarbons at reduced pressures were studied in a closed flame tube with hot-wire ignition. Characteristic two-lobe flammability-limit curves were exhibited by all the hydrocarbons studied. The minimum pressure limit was not affected by the molecular weight.
The rich limit, the lean limit, and the flammability range, when expressed as volume percent fuel, decreased as the number of carbon atoms increased. However, if the concentration of fuel is expressed as percent stoichiometric, the lean limit of the n-alkanes and n-alkenes attains a maximum value near a molecular weight of 75. Likewise the rich limit of the same two series attains a maximum near a molecular weight of 100. The flammability range, when expressed as volume percent fuel in the mixture, correlated with the molecular weight raised to the -0.70 power. The rich Limit correlated with the lean limit raised to the 0.56 power.
languageEnglish
titleNACA-RM-E52H15num
titlePressure limits of flame propagation of pure hydrocarbon-air mixtures at reduced pressureen
typestandard
page37
statusActive
treeNASA - National Aeronautics and Space Administration (NASA):;1952
contenttypefulltext
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DSpace software copyright © 2017-2020  DuraSpace
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