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Investigation of Instabilities and Heat Transfer Phenomena in Supercritical Fuels at High Heat Flux and TemperaturesA series of heated tube experiments was performed to investigate fluid instabilities that occur during heating of supercritical fluids. In these tests, JP-7 flowed vertically through small diameter tubes at supercritical pressures. Test section heated length, diameter, mass flow rate, inlet temperature, and heat flux were varied in an effort to determine the range of conditions that trigger the instabilities. Heat flux was varied up to 4 BTU/sq in./s, and test section wall temperatures reached as high as 1950 F. A statistical model was generated to explain the trends and effects of the control variables. The model included no direct linear effect of heat flux on the occurrence of the instabilities. All terms involving inlet temperature were negative, and all terms involving mass flow rate were positive. Multiple tests at conditions that produced instabilities provided inconsistent results. These inconsistencies limit the use of the model as a predictive tool. Physical variables that had been previously postulated to control the onset of the instabilities, such as film temperature, velocity, buoyancy, and wall-to-bulk temperature ratio, were evaluated here. Film temperatures at or near critical occurred during both stable and unstable tests. All tests at the highest velocity were stable, but there was no functional relationship found between the instabilities and velocity, or a combination of velocity and temperature ratio. Finally, all of the unstable tests had significant buoyancy at the inlet of the test section, but many stable tests also had significant buoyancy forces.
Document ID
20000085968
Acquisition Source
Glenn Research Center
Document Type
Preprint (Draft being sent to journal)
Authors
Linne, Diane L.
(NASA Glenn Research Center Cleveland, OH United States)
Meyer, Michael L.
(NASA Glenn Research Center Cleveland, OH United States)
Braun, Donald C.
(NASA Glenn Research Center Cleveland, OH United States)
Keller, Dennis J.
(RealWorld Quality Systems, Inc. Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
July 1, 2000
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NAS 1.15:210345
AIAA Paper 2000-3128
E-12392
NASA/TM-2000-210345
Report Number: NAS 1.15:210345
Report Number: AIAA Paper 2000-3128
Report Number: E-12392
Report Number: NASA/TM-2000-210345
Meeting Information
Meeting: Joint Propulsion
Location: Huntsville, AL
Country: United States
Start Date: July 16, 2000
End Date: July 19, 2000
Sponsors: American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics, American Society of Mechanical Engineers
Funding Number(s)
PROJECT: RTOP 523-61-13
Distribution Limits
Public
Copyright
Public Use Permitted.
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