Gas turbine engine and sensor multiple operating point analysis using optimization techniques

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

Volumn , Issue , 2000, Pages

  Gulati, A ^a   Zedda, M ^a   Singh, R ^a  

^a CRANFIELD UNIVERSITY   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; GAS TURBINES; GENETIC ALGORITHMS; PARAMETER ESTIMATION; PARETO PRINCIPLE;

ACCURATE ANALYSIS; COMPONENT PERFORMANCE; DIAGNOSTIC SYSTEMS; MULTIPLE OPERATING POINTS; OBJECTIVE FUNCTIONS; OPTIMIZATION TECHNIQUES; PARETO-OPTIMALITY; PERFORMANCE PARAMETERS;

BYPASS RATIO;

EID: 85085777074     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3716     Document Type: Conference Paper

References (14)

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10. rd Edition
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13. th Joint Propulsion Conference and Exhibit, June 20-24, Los Angeles, CA
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