RESEARCHING OF RELATIONS FORMING BETWEEN PARAMETERS OF TWO-SPOOL TURBOFAN DYNAMIC MODEL AND OPERATION MODE
Abstract
Keywords
Full Text:
PDF (Русский)References
Jaw, L. C., Mattingly, J. D. Aircraft engine controls: design, system analysis, and health monitoring. Reston, Virginia, USA, American institute of Aeronautics and Astronautics Ink. Publ., 2009. 385 p.
Richter, H. Advanced controls of turbofan engines. Springer Publ., 2011. 281 p.
Yepifanov, S. V., Kuznetsov, B. I. et al. Sintez sistem upravleniya i diagnostirovaniya gazoturbinnykh dvigateley [Synthesis of turbine engine automatic control and diagnostic systems]. Kiev, Tekhnika Publ., 1998. 312 p.
Kulikov, G. G., Goryunov, I. M., Romanov,M. A. Metod opredeleniya dinamicheskikh parametrov GTD v SAPR-D [Dynamic parameters determining GTD in Engine CAD]. Ispytaniye aviatsionnykh dvigateley : mezhvuz. nauchn. sb. – Testing of aircraft engines: interuniversity. scientific. Sat., Ufa, 1986, no. 14, pp. 39-46.
Volkov, D. I., Yepifanov, S. V. Sopryazheniye diapazonov zadaniya parametrov kvazilineynoy dinamicheskoy modeli GTD pri yeyo kusochno-lineynom predstavlenii [Ranges coordination of turbine engine peace-linear dynamic model parameters setting]. Vestnik dvigatelestroyeniya – Engine Herald, 2005, no. 2, pp. 67-71.
DOI: https://doi.org/10.32620/aktt.2020.7.13