A comparison of thermodynamic loss models applied to the J-79 turbojet engine

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Roth, B A ^a   Mavris, D N ^a  

^a Georgia Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FIGURE OF MERITS; FIGURES OF MERITS; THERMODYNAMIC LOSS; TURBINE PROPULSION; WORK LOSS;

PROPULSION;

EID: 84896481815     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (13)

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2. Clarke, J.M., Horlock, J.H., "Availability and Propulsion," J. Mech. Eng. Sci., v 17,No 4, 1975.
3. Curran, E.T., et al, "The Use of Stream Thrust Concepts for the Approximate Evaluation of Hypersonic Ramjet Engine Performance," Air Force Aero-propulsion Laboratry, Report AD-769 481, July 1973.
4. Riggins, D. W., "Evaluation of Performance Loss Methods for High-Speed Engines and Engine Components," Journal of Propulsion and Power, Vol. 13, No. 2, Mar-Apr 1997.
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7. Bejan, A., Advanced Engineering Thermodynamics, Wiley, New York, 1997.
8. Eight Decades of Progeress, A Heritage of Aircraft Turbine Technology, General Electric, Cincinnati, OH, 1990.
9. Neumann, G., Herman the German, William Morrow & Co., New York, 1984.
10. nd Ed., Haynes Publishing, Sparkford, N. Yeovil, UK, (ISBN 185260 5863)1997.
11. nd Ed., Wiley, New York, 1996.
12. Roth, B., and Mavris, D., "Analysis of Advanced Technology Impact on HSCT Engine Cycle Performance," AIAA99-2379.
13. Lewis, J.H., "Propulsive Efficiency from an Energy Utilization Standpoint," Journal of Aircraft, Vol. 13, No. 4, Apr 1976.