Open AccessSmall scale gas turbine combustor sizing
Author(s) -
Michał Czarnecki
Publication year - 2019
Publication title -
autobusy
Language(s) - English
Resource type - Journals
eISSN - 2450-7725
pISSN - 1509-5878
DOI - 10.24136/atest.2019.032
Subject(s) - combustor , sizing , scale (ratio) , gas turbines , combustion , turbine , engineering design process , mechanical engineering , process (computing) , computer science , gas burner , process engineering , engineering , physics , chemistry , organic chemistry , quantum mechanics , operating system
Presented article is focused on initial design of small scale combustors for micro scale jest engines. In comparison to the full size equivalent, small combustor are design and manufactured in experimental way. To try building universal numeric model for micro size design is important to acquire as many data as possible to identify boundary conditions for a model. Major advantage of analyzing different design is possibility to quick building prototype design without investigating complex process of combustion.