Numerical Simulation of High-Speed Civil Transport Inlet Operability with Angle of Attack

摘要: A high-speed civil transport inlet at Mach 2 and angle of attack is simulated by using a three-dimensional Navier‐Stokes solver with the Baldwin ‐Lomax algebraic turbulence model. An extrapolation uniform mass bleed boundary condition for slot successfully employed. At zero critical operation, computational pressure distribution agrees well experiment. The location intensity terminal shock total recovery are accurately computed. predicted steady-state distortion deviates from computed maximum that can sustain before unstart in good agreement Mesh ree nement results presented.