Dynamic of gas turbine engine gasdynamic stability loss
DOI:
https://doi.org/10.18372/2306-1472.25.1203Abstract
Dynamic of rotating stall and surge development in axial compressor after loss of gasdynamic stability is considered in the article. The Moore – Greitzer model is used for research. The model takes into account non-linear features of compressor characteristics and property of the compressor system. To determine system stabile state bifurcation analyze is carried out.
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