Joint prediction of aircraft gas turbine engine axial flow compressor off-design performance and surge line based on the expanded method of generalized functions
Russian aeronautics ; 57 , 3
2014
Aufsatz (Zeitschrift)
Englisch
BKL: | 55.50 Luftfahrzeugtechnik | |
Lokalklassifikation TIB: | 770/7040/8000 |
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