Full-annulus simulations of airfoil clocking in a 1-1/2 stage axial compressor

Proceedings of the ASME Turbo Expo

Volumn 1, Issue , 1999, Pages

  Dorney, D J ^a   Sondak, D L ^b   Cizmas, P G A ^c   Saren, V E ^d   Sevin, N M ^d  

^a VIRGINIA COMMONWEALTH UNIVERSITY   (United States)

^b BOSTON UNIVERSITY   (United States)

^c TEXAS A AND M UNIVERSITY   (United States)

^d CENTRAL INSTITUTE OF AVIATION MOTORS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; AXIAL FLOW TURBOMACHINERY; BOUNDARY LAYERS; CLOCKS; COMPRESSORS; GAS TURBINES; ROTORS (WINDINGS); STATORS; TURBINES; TURBOMACHINE BLADES; UNSTEADY FLOW; WAKES;

AXIAL COMPRESSORS; AXIAL TURBOMACHINES; COMPRESSOR EFFICIENCY; COMPUTATIONAL SIMULATION; COMPUTATIONAL WORK; HIGH-SPEED AXIAL COMPRESSORS; POTENTIAL EFFECTS; ROTOR AND STATORS;

AIRFOILS;

EID: 84928543482     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/99-GT-023     Document Type: Conference Paper

References (18)

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