Analytical modeling of turbine cascade leading edge heat transfer using skin friction and pressure measurements

Journal of Turbomachinery

Volumn 130, Issue 2, 2008, Pages

  Holley, Brian M ^a   Langston, Lee S ^a  

^a UNIVERSITY OF CONNECTICUT   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; AIRFOILS; BOUNDARY LAYER FLOW; CASCADES (FLUID MECHANICS); COMPUTATIONAL FLUID DYNAMICS; DYNAMICS; ELECTRIC GENERATORS; FLUID DYNAMICS; FLUID MECHANICS; FRICTION; GAS DYNAMICS; HEALTH; HEAT TRANSFER; HEATING EQUIPMENT; MOBILE TELECOMMUNICATION SYSTEMS; POTENTIAL FLOW; PRESSURE MEASUREMENT; SKIN; SKIN FRICTION; THERMOANALYSIS; TRIBOLOGY; TURBINES; WINGS;

A PLANE; ANALYTICAL MODELING; ANALYTICAL MODELLING; ANALYTICAL SOLUTIONS; CASCADE (CO); COMPUTATIONAL FLUID DYNAMICS (CFD) MODELING; CRITICAL LOCATION; FRICTION MEASUREMENTS; HIEMENZ FLOW; LEADING EDGE (LE); STAGNATION LINE; STAGNATION REGIONS; SURFACE PRESSURES; TURBINE CASCADES; UPPER BOUNDS;

HEAT EXCHANGERS;

EID: 47949098553     PISSN: 0889504X     EISSN: None     Source Type: Journal    
DOI: 10.1115/1.2812328     Document Type: Article

References (23)

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