International Journal of Aeronautical and Space Sciences
- Volume 1 Issue 1
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- Pages.36-47
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- 2000
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- 2093-274X(pISSN)
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- 2093-2480(eISSN)
Numerical Study of Three-Dimensional Compressible Flow Structure Within an S-Duct for Aircraft Engine Inlet
- Cho, Soo-Yong (Department of Aerospace and Mechanical Engineering Gyeongsang National University) ;
- Park, Byung-Kyu (Division of Thermal-fluid and Environmental Engineering Research Korea Institute Machinery and Materials)
- Published : 2000.05.01
Abstract
Three-dimensional compressible turbulent flow fields within the passage of a diffusing S-duct have been simulated by solving the Navier-Stokes equations with SIMPLE scheme. The average inlet Mach number is 0.6 and the Reynolds number based on the inlet diameter is