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Application of computational fluid dynamics to complex inlet ducts
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Schum, E. F. Towne, C. E. |
| Copyright Year | 1985 |
| Description | A three-dimensional parabolic Navier-Stokes code, PEPSIG, was used to analyze the flow in the subsonic diffuser section of a typical modern inlet design. The effect of curvature of the diffuser centerline and transitioning cross sections was studied to determine the primary cause of flow distortion in the duct. Total pressure values at the engine compressor face are reported. |
| File Size | 695915 |
| Page Count | 17 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19850021935 |
| Archival Resource Key | ark:/13960/t3518w69b |
| Language | English |
| Publisher Date | 1985-01-01 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics And Heat Transfer Navier-stokes Equation Ducted Flow Computational Fluid Dynamics Computation Engine Inlets Pressure Distribution Inlet Flow Compressible Flow Boundary Layers Computer Programs Viscous Flow Parabolic Differential Equations Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
