Predicting the performance of a gas turbine engine undergoing compressor blade erosion

39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2003, Pages

  Scala, Sinclaire M ^a   Konrad, Martin ^a   Mason, Robert B ^a   Skelton, Don ^b  

^a Concurrent Technologies Corporation ^*  (United States)

^b US Army Industrial Ecology Center   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT PROPULSION; COMPRESSIBILITY OF GASES; EFFICIENCY; EROSION; GAS TURBINES; SYSTEMS ENGINEERING; TURBOMACHINE BLADES;

COMPRESSOR BLADES; COMPRESSOR EFFICIENCY; DATA PROCESSORS; ENGINE PARAMETER; HELICOPTER ENGINES; OPERATING CONDITION; PARTICULATE MATTER; SHAFT HORSEPOWERS;

COMPRESSORS;

EID: 85085773673     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2003-5259     Document Type: Conference Paper

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