Конференції Національного Авіаційного Університету, AVIATION IN THE XXI-st CENTURY 2022

Розмір шрифту: 
Innovative ways of improving the characteristics of turbofan engine fans with a large and an ultra-large bypass ratio
Andrii Andriiovych Duliepov

Остання редакція: 2022-09-26

Ключові файли


turbofan engine, boundary layer control, active method, passive method, efficiency

Посилання


  1. Şöhret, Y. (2018). Ecologic performance and sustainability evaluation of a turbojet engine under on-design conditions. Aviation, 22(4), 166-173. https://doi.org/10.3846/aviation.2018.7085.
  2. D. Klein and C. Abeykoon, "Modelling of a turbojet gas turbine engine," 2015 Internet Technologies and Applications (ITA), 2015, pp. 200-206, doi: 10.1109/ITechA.2015.7317395.
  3. Raj K Vimal and G Dhanjayan 2018 IOP Conf. Ser.: Mater. Sci. Eng. 455 012035
  4. Fakhri Basher, M. 2022. Optimum Turbofan Engine Performance Through Variation of Bypass Ratio. Journal of Engineering and Sustainable Development. 17, 1 (May 2022), 138–153.
  5. Sun, Z. (2015). Micro Vortex Generators for Boundary Layer Control: Principles and Applications. International Journal of Flow Control, 7(1-2), pp. 67-86. doi:10.1260/1756-8250.7.1-2.67.
  6. M.L. Post, T. C. Corke, Separation Control on high angle of attack airfoil using plasma actuators, AIAA Journal, 2004, 42, 2177-2184.
  7. H. Babinsky, Y. Li, C. W. Pitt Ford, Microramp control of supersonic oblique shock-wave/boundary-layer interactions, AIAA Journal, 2009, 47, 668-675.