Modelling Thermal Conductivity Of Porous Thermal Barrier Coatings For High-Temperature Aero Engines Using Five Phase Model
| dc.contributor.author | Ghai, Ramandeep Singh | |
| dc.contributor.author | Chen, Kuiying | |
| dc.contributor.author | Baddour, Natalie | |
| dc.date.accessioned | 2018-11-09T15:00:22Z | |
| dc.date.available | 2018-11-09T15:00:22Z | |
| dc.date.issued | May-18 | |
| dc.description.abstract | Thermal Barrier Coatings (TBC) are used to shield hot sections of gas turbine engines, helping to prevent the melting of metallic surfaces. This paper proposes a Five-phase model to calculate the effective thermal conductivity of a TBC, taking into consideration the effect of various defects. By comparing the predicted values with experimental results, it was shown that the proposed five-phase model can predict the thermal conductivity of ceramic coatings closer to the actual values. | en_US |
| dc.identifier | CSME010 | |
| dc.identifier.isbn | 978-1-77355-023-7 | |
| dc.identifier.uri | http://hdl.handle.net/10315/35380 | |
| dc.identifier.uri | http://dx.doi.org/10.25071/10315/35380 | |
| dc.language.iso | en | en_US |
| dc.publisher | CSME-SCGM | en_US |
| dc.rights | The copyright for the paper content remains with the authors. | |
| dc.subject | Materials Technology | en_US |
| dc.subject | TBC | en_US |
| dc.subject | Thermal conductivity | en_US |
| dc.subject | High-temperature coatings | en_US |
| dc.subject | Modelling | en_US |
| dc.subject | Porosity and defects | en_US |
| dc.title | Modelling Thermal Conductivity Of Porous Thermal Barrier Coatings For High-Temperature Aero Engines Using Five Phase Model | en_US |
| dc.type | Article | en_US |