The thermal decomposition and heat transfer characteristics of gaseous, high-purity methane, several methane–hydrocarbon mixtures, and a typical natural gas fuel were evaluated using an electrically heated, stainless-steel tube test apparatus. Of several candidate heat transfer correlations, the Dittus–Boelter heat transfer correlation provided the best fit of the methane heat transfer data over the range of Reynolds numbers 10,000 to 215,000. The thermal stability (i.e., deposit formation) characteristics of the methane–hydrocarbon mixtures and the natural gas fuel were established and compared with the deposition characteristics of high-purity methane. Testing was conducted at wall temperatures up to 900 K (fuel temperatures to 835 K) for durations of up to 60 hours. Measurements of deposit mass indicated that there was essentially no deposit buildup for wall temperatures below 650 K. Deposit began to form at wall temperatures between 650 K and 775 K. Above 775 K, there was a rapid monotonic increase in deposition. The data suggest that the use of high-purity methane instead of natural gas at temperatures above 775 K could reduce the deposit thickness under similar operating conditions by as much as a factor of three, or permit operation at correspondingly higher temperatures.

1.
Back, M. H., and Back, R. A., 1983, “Thermal Decomposition and Reactions of Methane,” in: Pyrolysis—Theory and Industrial Practice, Academic Press, New York.
2.
Edwards, T., 1992, “Deposition During Vaporization of Jet Fuel in a Heated Tube,” 30th AIAA Aerospace Sciences Meeting, Reno, NV, Jan. 6–9.
3.
Ely, J. F., and Huber, M. L., 1990, “NIST Standard Reference Database 4—NIST Thermophysical Properties of Hydrocarbon Mixtures Database,” Version 1.0.
4.
Heneghan
S. P.
,
Martel
C. R.
,
Williams
T. F.
, and
Ballal
D. R.
,
1993
, “
Studies of Jet Fuel Thermal Stability in a Flowing System
,”
ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER
, Vol.
115
, pp.
480
485
.
5.
Holman, J. P., 1981, Heat Transfer, 5th ed., McGraw-Hill, New York.
6.
Joslin, C. L., 1968, “The Potential of Methane as a Fuel for Advanced Aircraft,” presented at the ASME Aviation and Space Conference, June.
7.
Marteney
P. J.
, and
Spadaccini
L. J.
,
1986
, “
Thermal Decomposition of Aircraft Fuels
,”
ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER
, Vol.
108
, pp.
648
653
.
8.
Mechanical Engineering Staff
,
1986
, “
Propelling the Aerospace Plane
,”
Mechanical Engineering
, Vol.
108
, No.
6
, pp.
32
36
.
9.
Nishiyama
Y.
, and
Tamai
Y.
,
1980
, “
Wall Effects During Thermal Reactions
,”
CHEMTECH
, Vol.
10
, No.
11
, pp.
680
684
.
10.
Taylor
W. F.
,
1974
, “
Deposit Formation From Deoxygenated Hydrocarbons, Part I—General Features
,”
Ind. & Eng. Chem., Prod. Res. & Devel.
, Vol.
13
, No.
2
, pp.
133
138
.
This content is only available via PDF.
You do not currently have access to this content.