Flow and heat transfer in a ribbed U-duct under typical engine conditions

Proceedings of the ASME Turbo Expo

Volumn 4, Issue , 1998, Pages

  Shih, T I P ^a   Lin, Y L ^a   Stephens, M A ^a   Chyu, M K ^a   Civinskas, K C ^b  

^a CARNEGIE MELLON UNIVERSITY   (United States)

^b NASA GLENN RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COOLANTS; DUCTS; FINITE VOLUME METHOD; HEAT TRANSFER; HYDRAULIC MOTORS; NAVIER STOKES EQUATIONS; OCEANOGRAPHY; REYNOLDS NUMBER; TURBULENT FLOW;

ALTERNATING DIRECTION IMPLICIT SCHEMES; COMPRESSIBLE NAVIER-STOKES; CONSERVATION EQUATIONS; EXPLICIT ALGEBRAIC REYNOLDS STRESS MODELS; FLOW AND HEAT TRANSFER; FLUX DIFFERENCE SPLITTING; INDUSTRIAL GAS TURBINES; THREE-DIMENSIONAL FLOW;

GAS TURBINES;

EID: 84973167214     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/98-GT-213     Document Type: Conference Paper

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