Spray characteristics like mean drop diameter and spray cone angle play an important role in the process of combustion within a gas turbine combustor. In order to study their effects on wall and exit temperature distributions and combustion efficiency in the combustor, a numerical model of a typical
β¦ LIBER β¦
Combustion performance of hydrogen in a small gas turbine combustor
β Scribed by P. Sampath; F. Shum
- Publisher
- Elsevier Science
- Year
- 1985
- Tongue
- English
- Weight
- 591 KB
- Volume
- 10
- Category
- Article
- ISSN
- 0360-3199
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## Abstract The development of abradeable gas turbine seals for higher temperature duties has been the target of an EUβfunded R&D project, ADSEALS, with the aim of moving towards seals that can withstand surface temperatures as high as βΌ 1100Β°C for periods of at least 24,000 h. The ADSEALS project