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NASA NTRS · 20040120931

High Reynolds Number Thermal Stability Experiments

Abstract

This work represents preliminary thermal stability results for liquid hydrocarbon fuels. High Reynolds Number Thermal Stability experiments with Jet A and RP-1 resulted in a quantitative measurement of the thermal stability. Each fuel flowed through a heated capillary tube that held the outlet temperature at 290 C. An optical pyrometer measured the surface temperature of the tube at 12 locations as a function of time. The High Reynolds Number Thermal Stability number was then determined using standards published by the American Society for Testing and Materials. The results for Jet A showed lower thermal stability than similar tests conducted at another facility. The RP-1 results are the first reported using this technique. Because the temperature rise on the capillary tube during testing for the RP-1 fuels was not significant, a new standard for the testing conditions should be developed for these types of fuels.

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BibTeXRIS

Emens, Jessica M., Brown, Sarah P., Frederick Robert A., Jr., Wood, A. John. 2004-07-11. High Reynolds Number Thermal Stability Experiments. https://ntrs.nasa.gov/citations/20040120931

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