The Development of an Aviation Fuel Thermal Stability Test Unit
Author:
Affiliation:
1. Rolls-Royce Inc., Engineering, Atlanta, GA 30339
2. Rolls-Royce PLC, Engineering, Derby, United Kingdom
3. Aircraft Division, Naval Air Warfare Center, Trenton, NJ 08628
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/117/3/468/5889106/468_1.pdf
Reference8 articles.
1. Chin J. , and LefebvreA., 1992, “Experimental Techniques for the Assessment of Fuel Thermal Stability,” Journal of Propulsion and Power, Vol. 8, No. 6, pp. 3–4.
2. Goodman, H., and Bradley, R., 1970, “High Temperature Hydrocarbon Fuels Research in an Advanced Aircraft Fuel System Simulator,” Technical Report AFAPL–TR–70–13, WPAFB, OH, p. 109, Fig. 3.
3. Goodyear, E., and Vere, R., 1985, Aviation Fuels Technology, Macmillan Publishers LTD, London, United Kingdom.
4. Hazlett, R., 1991, “Thermal Oxidation Stability of Aviation Turbine Fuels,” ASTM Publication 31–001092–12, Philadelphia, PA.
5. Heneghan S. P. , MartelC. R., WilliamsT. F., and BallalD. R., 1995, “Effects of Oxygen and Additives on the Thermal Stability of Jet Fuels,” ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER, Vol. 117, 1995, pp. 120–124.
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