Digital simulator for steady-state performance prediction of military turbofan engine

Journal of Propulsion and Power

Volumn 14, Issue 1, 1998, Pages 74-81

  Sanghi, Vivek ^a   Lakshmanan, B K ^a   Sundararajan, V ^a  

^a GAS TURBINE RESEARCH ESTABLISHMENT   (India)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; COMPUTER SIMULATION; MILITARY AIRCRAFT;

ENGINE CYCLE REDESIGNING; PERFORMANCE PREDICTION; TWIN SPOOL TURBOFAN ENGINES;

TURBOFAN ENGINES;

EID: 0031672454     PISSN: 07484658     EISSN: 15333876     Source Type: Journal    
DOI: 10.2514/2.5252     Document Type: Article

References (6)

1. Sanghi, V., "Computer Aided Conceptual Design of Propulsion System for Combat Aircraft," Ph.D. Dissertation, Indian Inst. of Technology, Bombay, India, 1996.
2. "Gas Turbine Engine Steady State Performance Presentation for Digital Computer Programs," Society of Automotive Engineers, Aerospace Recommended Practice, 681, 1989.
3. Cohen, H., Rogers, G. F. C., and Saravanamutto, H. I. H., "Gas Turbine Theory," 3rd ed., Longman Scientific & Technical, London, 1987.
4. Palsane, S., Lakshmanan, B. K., and Sundararajan, V., "Convergent Divergent Nozzle Modeling for Kaveri Engine," Gas Turbine Research Establishment, ITM/ES-8709, Bangalore, India, April 1994.
5. Fawke, A. J., and Saravanamutto, H. I. H., "Digital Computer Methods for Prediction of Gas Turbine Dynamic Response," Society of Automotive Engineers, Paper 710550, June 1971.
6. Palsane, S., Lakshmanan, B. K., and Sundararajan, V., "Design Document on Kaveri Engine Simulation," Gas Turbine Research Establishment, ITM/ES-8704, Bangalore, India, Nov. 1991.