Superior disturbance resistance
With an external compression angle, this inlet/isolator maintains uniform outlet flow and exhibits significantly reduced variations in total pressure recovery coefficient under varying incoming boundary layer thicknesses, providing stable conditions for downstream combustion.
Fu-Min, Zeng · Yanliang, Yang · Guo, Guangming · Hao, Chen
Journal of Aeronautics, Astronautics and Aviation, Series A 2026
At 10° compression angle, variations in total pressure recovery coefficient are smaller under different boundary layer thicknesses
Outlet flow field of isolator is more uniform