Mathematical model describing the coupled heat transfer in effusion cooled combustor walls

Proceedings of the ASME Turbo Expo

Volumn 3, Issue , 1997, Pages

  Mutiny, M ^a   Schulz, A ^a   Wittig, S ^a  

^a UNIVERSITY OF KARLSRUHE   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT ENGINES; COMBUSTORS; COOLANTS; GAS TURBINES; TEMPERATURE;

COLD SIDE; COUPLED HEAT TRANSFER; DIMENSIONLESS PARAMETERS; EXIT TEMPERATURE; FILM COOLING; HEAT BALANCE; HEAT EXCHANGE; PARAMETER STUDIES;

HEAT TRANSFER;

EID: 84973652319     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1115/97-GT-329     Document Type: Conference Paper

References (7)

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2. Wadia Alt, Nealy D.A. "Development of a Design Model for Airfoil Leading Edge Film Cooling", ASME Paper 85-GT-120
3. Kumada M., Hirata M., Icasagi N. "Studies of Full Coverage Film cooling Part 2: Measurements of Local Heat Transfer Coefficient", ASME Paper 81-GT-38, 1981
4. Martiny M., Schulz A., Wittig S.: "Full Coverage Film Cooling Investigations: Adiabatic Wall Temperatures and Flow Visualization", ASME Paper 95-WA/HT-4, 1995
5. Choc H., Kays W.M., Moffat RI, "The Superposition Approach to Film Cooling", ASME Paper 74-WA/HAT-27
6. Waterloo Maple Software and University of Waterloo, "MAPLE V Release 3", 1994
7. Microsoft Corporation, "Microsoft Excel 5.0c", Copyright 1985-1994