Consequences of aero-engine deteriorations for military aircraft

Applied Energy

Volumn 70, Issue 2, 2001, Pages 103-133

  Naeem, M ^a   Singh, R ^b   Probert, D ^b  

^a School of Avionics and Electrical Engineering   (Pakistan)

^b CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; DECISION MAKING; ECONOMIC AND SOCIAL EFFECTS; FUEL CONSUMPTION; GAS TURBINE LOCOMOTIVES;

AERO-ENGINE DETERIORATIONS;

MILITARY AIRCRAFT;

AIRCRAFT; ENGINEERING;

EID: 0035479051     PISSN: 03062619     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0306-2619(01)00028-9     Document Type: Article

References (23)

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4. A preliminary assessment of compressor fouling
5. Simulation of an advanced twin-spool industrial gas-turbine
6. Results of experiments for determining the influence of blade-profile changes and manufacturing tolerances on efficiency, the enthalpy drop and the mass flow of multi-stage axial turbines
7. The influence of the blading-surfaces' roughness on the aerodynamics behavior and characteristics of an axial compressor
8. Operating experience for residual fuel-oil with a W251 combustion turbine
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13. Implications of engine deterioration for a high-pressure turbine blade's low-cycle fatigue-life consumption
14. Implications of engine deterioration for an aero-engine HP turbine blade's thermal-fatigue life
15. Effects of cycle choice and deterioration on thrust indicators for civil engines
16. Implications of engine deterioration for operational effectiveness of a military aircraft
17. Implications of engine deterioration for fuel usage