Computational investigation of flow through a louvered inlet configuration

Date

2001-01-01

Author

Tuncer, İsmail Hakkı

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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.

Subject Keywords

Applied aerodynamics

URI

https://hdl.handle.net/11511/56429

DOI

https://doi.org/10.2514/6.2001-2477

Conference Name

19th AIAA Applied Aerodynamics Conference

Collections

Department of Aerospace Engineering, Conference / Seminar

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Citation Formats

İ. H. Tuncer, “Computational investigation of flow through a louvered inlet configuration,” presented at the 19th AIAA Applied Aerodynamics Conference, Anaheim,CA,U.S.A., 2001, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/56429.