The Effects of Ribs and Tip Wall Distance on Heat Transfer for a Varying Aspect Ratio Two-Pass Ribbed Internal Cooling Channel

Journal of Turbomachinery

Volumn 135, Issue 2, 2012, Pages

  Jenkins, Sean C ^a   Zehnder, Frank ^a   Shevchuk, Igor V ^a   von Wolfersdorf, Jens ^a   Weigand, Bernhard ^a   Schnieder, Martin ^b  

^a UNIVERSITY OF STUTTGART   (Germany)

^b ALSTOM   (France)

Author keywords

[No Author keywords available]

Indexed keywords

BEND EFFECT; BLADE TIP; COOLING CHANNELS; GAS TURBINE BLADES; HEAT TRANSFER CHARACTERISTICS; HEAT TRANSFER MEASUREMENTS; INTERNAL COOLING; PRESSURE LOSS; SPATIALLY RESOLVED; THERMOCHROMIC LIQUID CRYSTALS; TRAILING EDGES; VARYING THICKNESS; WALL DISTANCES;

ASPECT RATIO; COMPUTATIONAL FLUID DYNAMICS; LIQUID CRYSTALS; SERPENTINE;

HEAT TRANSFER;

EID: 84868274684     PISSN: 0889504X     EISSN: 15288900     Source Type: Journal    
DOI: 10.1115/1.4006584     Document Type: Article

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