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Alternative fuels for aviation

Published online by Cambridge University Press:  04 July 2016

E. M. Goodger*
Affiliation:
Cranfield Institute of Technology

Extract

Aviation is an advanced technology, constantly pursuing higher performance, and backed by painstaking research into new materials and techniques. The target of “performance” has changed with the period, but the extent to which energy can be provided for propulsion has always been rated of major importance. Since propulsive energy is stored on board in a fuel medium, the more obvious criteria for the fuel are the energy density (based on mass and/or volume) and the proportion of this energy usable within the propulsion system. At the same time, the fuel must respond safely to reasonable handling procedures. The more subtle requirements to emerge over recent years include those of a minimum potential for pollutant formation and, in the case of very high speed flight, a maximum capacity for heat absorption.

Type
Research Article
Copyright
Copyright © Royal Aeronautical Society 1975 

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References

1. Goodger, E. M. Hydrocarbon fuels. Macmillan, London. To be published.Google Scholar
2. Churchill, A. V. Characteristics of advanced military turbine fuels. Jet Fuel Quality Symposium, San Antonio, Texas, October 1968.Google Scholar
3. Dukek, W. G. Selected hydrocarbons as high performance fuels. American Chemical Society, Symposium on High Energy Fuels, Philadelphia, USA, 25th February 1960.Google Scholar
4. Anon. Shelldyne. Shell International Petroleum Co Ltd, London, April 1965.Google Scholar
5. Anon. Borane Technical Bulletins. Callery Chemical Co, Pittsburgh 37, USA.Google Scholar
6. Wilson, W. E. and Berl, W. G. Ramjet technology. Chapter 6—Fuels. Tech Memo TG 610-6. The Johns Hopkins University, USA, July 1965.Google Scholar
7. Anon. Rocket engine propellants. Rocketdyne, Canoga Park, California, USA, 1959.Google Scholar
8. Goodger, E. M. Rocket and other fuels. Section A9, The efficient use of energy. IPC Science and Technology Press. To be published.Google Scholar
9. Fultz, J. R. Future airforce requirements for hydrocarbon fuels. Tech Report ASD TR 61-728. Air Force Systems Command, May 1962.Google Scholar
10. NASA Tech Note TND-3471,1967.Google Scholar
11. Brewer, G. D. The case for hydrogen fueled transport aircraft. AIAA Paper No 73-1323, April 1974.Google Scholar
12. Bruning, H. C. A. M., Kuypers, F. A. and van Vucht, J. H. N. Reversible room-temperature absorption of large quantities of hydrogen by intermetallic compounds. Philips Research Report 25, April 1970.Google Scholar
13. Drell, I. L. and Belles, F. E. Survey of hydrogen combustion properties. NACA Report R 1383, 1958.Google Scholar
14. Small, W. J., Fetterman, D. E. and Bonner, T. F. Alternate fuels for transportation—Part 1, hydrogen for aircraft. Mechanical Engineering, 18, Vol 96, No 5, May 1974.Google Scholar
15. Lewis Laboratory Staff. Hydrogen for turbojet and ramjet powered flight. NACA RM E57D23, 26th April 1957.Google Scholar
16. Austin, A. L. and Sawyer, R. F. The hydrogen fuel economy and aircraft propulsion. AIAA Paper No 73- 1319, April 1974.Google Scholar
17. Morgan, M. B. Supersonic aircraft—promise and problems. Journal of the RAeS, Vol 64, p 315, 1960.Google Scholar