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naca-tn-2549

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National Advisory Committee for Aeronautics, Technical Notes - Investigation of Hydrocarbon Ignition

Accurate spontaneous ignition temperatures have been determined
for some 50 pure organic compounds. The effects of a wide variety
of additives and of eight selected metals on the spontaneous—ignitionr
temperature values of representatives of this group also have been
observed. Results are correlated with chemical structure and with
antiknock characteristics where known; more fundamental aspects of
the possible chainrbreaking and chain—branching reactions involved
also are considered.

While considerable data are available on the spontaneous ignition
temperatures of Organic compounds, there is wide discrepancy between
the results of various investigators, and even within the findings of
a single investigator. This difficulty is due to the marked sen—
sitivity of the determinations to a large number of variables, as has
been pointed out previously (reference 1), and, accordingly, to even
minor variations in equipment or procedure. The present study has as
its objective: (1) The determination of a large number of spontaneous—
ignition—temperature values for selected series of organic comp
pounds of high purity in order to correlate structure with ease of
spontaneous flammability, (2) the observation of the effect of metal
surfaces and of a variety of additives on the spontaneous—ignition—
temperature values of certain hydrocarbons, and (3) the development
of sufficient information and theory to permit a more scientific
approach to the formulation of fuels and lubricants of reduced sponr
taneous flammability. This study was made at the Applied Science
Research Laboratory of the University of Cincinnati under the sponsor-
ship and with the financial assistance of the National Advisory
Committee for Aeronautics.

The equipment for this investigation comprised two metal blocks
(one stainless steel and one copper) modeled after the apparatus of
Sortman, Beatty, and Heron (reference 2). The two blocks gave comr
pletely parallel results; however, the copper block was not used at
the higher temperatures because of the rapid formation of a heavy
copper—oxide layer under those conditions.

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naca-tn-2549

  • Version
  • 102 Downloads
  • 1.35 MB File Size
  • 1 File Count
  • January 9, 2017 Create Date
  • January 9, 2017 Last Updated
Scroll for Details

National Advisory Committee for Aeronautics, Technical Notes - Investigation of Hydrocarbon Ignition

Accurate spontaneous ignition temperatures have been determined
for some 50 pure organic compounds. The effects of a wide variety
of additives and of eight selected metals on the spontaneous—ignitionr
temperature values of representatives of this group also have been
observed. Results are correlated with chemical structure and with
antiknock characteristics where known; more fundamental aspects of
the possible chainrbreaking and chain—branching reactions involved
also are considered.

While considerable data are available on the spontaneous ignition
temperatures of Organic compounds, there is wide discrepancy between
the results of various investigators, and even within the findings of
a single investigator. This difficulty is due to the marked sen—
sitivity of the determinations to a large number of variables, as has
been pointed out previously (reference 1), and, accordingly, to even
minor variations in equipment or procedure. The present study has as
its objective: (1) The determination of a large number of spontaneous—
ignition—temperature values for selected series of organic comp
pounds of high purity in order to correlate structure with ease of
spontaneous flammability, (2) the observation of the effect of metal
surfaces and of a variety of additives on the spontaneous—ignition—
temperature values of certain hydrocarbons, and (3) the development
of sufficient information and theory to permit a more scientific
approach to the formulation of fuels and lubricants of reduced sponr
taneous flammability. This study was made at the Applied Science
Research Laboratory of the University of Cincinnati under the sponsor-
ship and with the financial assistance of the National Advisory
Committee for Aeronautics.

The equipment for this investigation comprised two metal blocks
(one stainless steel and one copper) modeled after the apparatus of
Sortman, Beatty, and Heron (reference 2). The two blocks gave comr
pletely parallel results; however, the copper block was not used at
the higher temperatures because of the rapid formation of a heavy
copper—oxide layer under those conditions.

FileAction
naca-tn-2549 Investigation of Hydrocarbon Ignition.pdfDownload 
17,005 Documents in our Technical Library
2727296 Total Downloads

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Newest Additions

NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
NASA-RP-1060 Subsonic Aircraft: Evolution and the Matching of Size to Performance
AA-CP-20212-001
AA-CP-20212-001
ADPO10769 Occurrence of Corrosion in Airframes
The purpose of this lecture is to provide an overview ...
MIL-STD-1759 Rivets and Rivet Type Fasteners Preferred for Design
The purpose of this book form standard is to provide ...
MIL-STD-810G Environmental Engineering Considerations and Laboratory Tests
This standard contains materiel acquisition program planning and engineering direction ...