Probabilistic design for blade-tip radial running clearance of HPT

Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics

Volumn 39, Issue 3, 2013, Pages 305-309

  Fei, Chengwei ^a   Bai, Guangchen ^a   Zhao, Heyang ^a   Han, Yanbin ^a  

^a BEIHANG UNIVERSITY   (China)

Author keywords

Aeroengine; Blade tip radial running clearance (BTRRC); High pressure turbine(HPT); Probabilistic design; Response surface method(RSM); Sensitivity analysis

Indexed keywords

AERO-ENGINE; BLADE-TIP RADIAL RUNNING CLEARANCE (BTRRC); HIGH PRESSURE TURBINE; PROBABILISTIC DESIGN; RESPONSE SURFACE METHOD;

AIRCRAFT ENGINES; DEFORMATION; DESIGN; PROBABILITY DISTRIBUTIONS; SENSITIVITY ANALYSIS; TURBOMACHINE BLADES;

TURBINE COMPONENTS;

EID: 84877133674     PISSN: 10015965     EISSN: None     Source Type: Journal    
DOI: None     Document Type: Article

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