Computational investigation of blade slotting on a high-load low-pressure turbine profile at various reynolds numbers: Part I-Slotting scheme's verification

Journal of Thermal Science

Volumn 20, Issue 1, 2011, Pages 13-20

  Du, Qiang ^a,b   Zhu, Junqiang ^a   Zhou, Min ^a,c   Li, Wei ^a,b  

^a INSTITUTE OF ENGINEERING THERMOPHYSICS   (China)

^b UNIVERSITY OF CHINESE ACADEMY OF SCIENCES   (China)

^c AVIC Manufacturing Technology Institute   (China)

Author keywords

Boundary layer separation and reattachment; High aerodynamic loading LP turbine blade; Slotted blade

Indexed keywords

AERO-ENGINE; AERODYNAMIC LOADING; BOUNDARY-LAYER SEPARATION; COMPUTATIONAL INVESTIGATION; COMPUTATIONAL RESULTS; HIGH ALTITUDE; LOW REYNOLDS NUMBER; LOW-PRESSURE TURBINES; LP TURBINES; PROFILE LOSS; SEPARATION BUBBLE; SLOTTED-BLADE; TURBINE AIRFOILS;

AERODYNAMIC LOADS; AERODYNAMICS; AIRFOILS; BOUNDARY LAYERS; COMPUTATIONAL GEOMETRY; FLIGHT ENVELOPES; LOADING; REYNOLDS NUMBER; SLOTTING; TURBINES;

TURBOMACHINE BLADES;

EID: 79952774012     PISSN: 10032169     EISSN: None     Source Type: Journal    
DOI: 10.1007/s11630-011-0428-y     Document Type: Article

References (9)

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