Application of reduced-order aerodynamic modeling to the analysis of structural uncertainty in bladed disks

American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) IGTI

Volumn 5 B, Issue , 2002, Pages 1257-1265

  Willcox, K ^a   Peraire, J ^a  

^a MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

BLADED DISKS; HIGH ORDER COMPUTATIONAL FLUID DYNAMICS; ORTHOGONAL DECOMPOSITION TECHNIQUE;

AERODYNAMICS; COMPUTATIONAL FLUID DYNAMICS; STRUCTURAL ANALYSIS; TIME DOMAIN ANALYSIS; TURBOMACHINE BLADES;

DISKS (MACHINE COMPONENTS);

EID: 0037002943     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/GT2002-30680     Document Type: Conference Paper

References (23)

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