Dynamic behavior of the gas turbine engine regenerator with complanar channels
- Authors: Trushin V.1
-
Affiliations:
- Ufa State Aviation Technical University
- Issue: Vol 60, No 2 (2017)
- Pages: 312-316
- Section: Aircraft and Rocket Engine Theory
- URL: https://journal-vniispk.ru/1068-7998/article/view/230148
- DOI: https://doi.org/10.3103/S1068799817020246
- ID: 230148
Cite item
Abstract
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.
About the authors
V.A. Trushin
Ufa State Aviation Technical University
Author for correspondence.
Email: at-t@ugatu.ac.ru
Russian Federation, ul. Karla Marksa 12, Ufa, 450008 Bashkortostan
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