Simplified thrust and fuel consumption models for modern two-shaft turbofan engines

Journal of Aircraft

Volumn 45, Issue 4, 2008, Pages 1450-1456

  Battel, Matthias ^a,c,d   Young, Trevor M ^b,d  

^a Department of Compressors   (Germany)

^b UNIVERSITY OF LIMERICK   (Ireland)

^c Performance Department

^d AIAA ^*

Author keywords

[No Author keywords available]

Indexed keywords

ENGINES;

EMPIRICAL CONSTANTS; EMPIRICAL EQUATIONS; ENGINE PERFORMANCE; PERFORMANCE ANALYSIS; PERFORMANCE DATA; THRUST MODELING; THRUST SPECIFIC FUEL CONSUMPTION; THRUST VARIATIONS;

TURBOFAN ENGINES;

EID: 49349090286     PISSN: 00218669     EISSN: 15333868     Source Type: Journal    
DOI: 10.2514/1.35589     Document Type: Conference Paper

References (11)

1. Torenbeek, E., Synthesis of Subsonic Airplane Design, Delft Univ. Press, Delft, The Netherlands, 1982.
2. Anderson, J. D., Jr., Airplane Performance and Design, McGraw-Hill, New York, 1999.
3. Eshelby, M. E., Airplane Performance: Theory and Practice, Arnold, London, 2000.
4. Asselin, M., Introduction to Aircraft Performance, AIAA, Reston, VA, 1997.
5. Ojha, S. K., Flight Performance of Airplane, AIAA, Reston, VA, 1995.
6. Raymer, D., Airplane Design: A Conceptual Approach, 4th. ed., AIAA, Reston, VA, 2006.
7. Howe, D., Aircraft Conceptual Design Synthesis, Professional Engineering Publishing, London, 2000.
8. Mair, W. A., and Birdsall, D. L., Aircraft Performance, Cambridge Univ. Press, Cambridge, England, U.K., 1992.
9. "Approximate Methods for Estimation of Cruise Range and Endurance: Aeroplanes With Turbo-jet and Turbo-Fan Engines," IHS ESDU International, ESDU 73019, 1982.
10. Martinez-Val, R., and Perez, E., "Optimum Cruise Lift Coefficient in Initial Design of Jet Aircraft," Journal of Aircraft, Vol. 29, No. 4, 1992, pp. 712-714.
11. Braeunling, W., Flugzeugtriebwerke, Springer-Verlag, Heidelberg, Germany, 2001.