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High Reynolds Number Thermal Stability ExperimentsThis 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.
Document ID
20040120931
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Emens, Jessica M.
(Alabama Univ. Huntsville, AL, United States)
Brown, Sarah P.
(Alabama Univ. Huntsville, AL, United States)
Frederick Robert A., Jr.
(Alabama Univ. Huntsville, AL, United States)
Wood, A. John
(Stanhope-Seta Surrey, United Kingdom)
Date Acquired
September 7, 2013
Publication Date
July 11, 2004
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
AIAA Paper 2004-4089
Report Number: AIAA Paper 2004-4089
Meeting Information
Meeting: AIAA Joint Propulsion Conference
Location: Fort Lauderdale, FL
Country: United States
Start Date: July 11, 2004
End Date: July 14, 2004
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC8-200
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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