Quantitative influence of the steady non-reflecting boundary conditions on blade-to-blade computations

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 2000, Pages

  Contreras, Jesus ^a   Corral, Roque ^b  

^a Industria de TurboPropulsores SA   (Spain)

^b Technical University of Madrid UPM   (Spain)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AIRCRAFT PROPULSION; FLOW FIELDS;

LPT BLADE; NON REFLECTING BOUNDARY CONDITION; OUTFLOW BOUNDARY CONDITIONS; QUANTITATIVE INFLUENCE; SECOND ORDERS; UNSTRUCTURED CODES;

BOUNDARY CONDITIONS;

EID: 84955135149     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/2000-GT-0515     Document Type: Conference Paper

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