Flow mechanism for stall margin improvement due to circumferential casing grooves on axial compressors

Proceedings of the ASME Turbo Expo 2004

Volumn 5 A, Issue , 2004, Pages 557-569

  Shabbir, Aamir ^a   Adamczyk, John J ^b  

^a UNIVERSITY OF TOLEDO   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTATIONAL METHODS; PRESSURE EFFECTS; TENSORS; TURBULENCE; VELOCITY; VISCOSITY;

AXIAL MOMENTUM; MASS FLOW; RADIAL COORDINATES; STRESS TENSORS;

COMPRESSORS;

EID: 10244264763     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/gt2004-53903     Document Type: Conference Paper

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