Dynamic behavior of the gas turbine engine regenerator with complanar channels
- Авторлар: Trushin V.1
-
Мекемелер:
- Ufa State Aviation Technical University
- Шығарылым: Том 60, № 2 (2017)
- Беттер: 312-316
- Бөлім: Aircraft and Rocket Engine Theory
- URL: https://journals.rcsi.science/1068-7998/article/view/230148
- DOI: https://doi.org/10.3103/S1068799817020246
- ID: 230148
Дәйексөз келтіру
Аннотация
This paper expounds a technique for calculating unsteady gas temperatures, air and heat transfer elements of the corrugated plate of a recuperative heat exchanger with complanar channels for start and shut-off modes of the regenerative turbine engine. Under consideration are the distribution of thermal stresses in the plate, heat exchanger service life under stationary conditions, and the allowable number of dynamic “start–shut-off” cycles.
Негізгі сөздер
Авторлар туралы
V.A. Trushin
Ufa State Aviation Technical University
Хат алмасуға жауапты Автор.
Email: at-t@ugatu.ac.ru
Ресей, ul. Karla Marksa 12, Ufa, 450008 Bashkortostan
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