Akademik Veri Yönetim Sistemi
19th AIAA Applied Aerodynamics Conference 2001, Anaheim, CA, Amerika Birleşik Devletleri, 11 - 14 Haziran 2001
Viscous, subsonic flows through a flush louvered inlet configuration without inlet vanes are investigated using the overflow Navier-Stokes solver with overset grids. The variation of the mass flow rate through the engine intake as a function of intake pressure is assessed. The computed results show that the flow distortion and the pressure loss in the plenum chamber are significant, yet a sufficient amount of mass flow rate may be obtained at the expense of total pressure recovery.