A conjugate heat transfer model for heat load prediction in combustion devices

Summary, in English

Different phenomena such as complex flow field and heat release by combustion are involved in the heat transfer process in combustion chambers. This paper concerns prediction of heat load and wail temperature in a gas turbine combustor by taking different phenomena into account. Two dimensional axi-symmetric models were used to model the flow field and combustion in a premised combustor with two different cooling schemes. The k-ε turbulence model and Eddy Dissipation Concept (EDC) were used for modeling turbulent flow and combustion, respectively. In the modeling of heat transfer through the walls, a conjugate heat transfer formulation was applied. The temperatures calculated by the models were compared with experimental data. The results showed that although worse agreement was found in some parts, however generally the trends of the temperature variations predicted very well. In addition, radiative heat transfer has been included in the study. The results showed that radiative heat transfer in simple and ribbed duct cooling schemes can increase the average inner wall temperature by to 33 and 40 K, respectively.

• Author: Mehdi Bahador; Bengt Sundén
• Department/s: Heat Transfer
• Publishing year: 2006
• Language: English
• Pages: 1813-1819
• Publication/Series: Collection of Technical Papers - 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference Proceedings
• Volume: 3
• Links: http://aiaa.org/agenda.cfm?lumeetingid=1190&formatview=1&dateget=07-Jun-06
• Document type: Conference paper
• Publisher: American Institute of Aeronautics and Astronautics
• Topic: Energy Engineering
• Keywords: Gas turbine combustors; Eddy Dissipation Concept (EDC); Ribbed duct cooling; Radiative heat transfer
• Conference name: 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference Proceedings
• Conference date: 2006-06-05 - 2006-06-08
• Conference place: San Francisco, CA, United States
• Status: Published