Development of an Augmented Conceptual Design Tool for Aircraft Gas Turbine Combustors
Combustor design is the most unreliable and challenging portion in the design process of a gas turbine. To ensure the proper performance, many experimental tests must be performed on a combustor in the industry. The above mentioned design phase is costly and time consuming. This paper focused on an...
| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
MULTIPHYSICS
2016-03-01
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| Series: | International Journal of Multiphysics |
| Online Access: | http://journal.multiphysics.org/index.php/IJM/article/view/56 |