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An lu implicity scheme for high speed inlet analysis
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Jameson, A. Yoon, S. |
| Copyright Year | 1986 |
| Description | A numerical method is developed to analyze the inviscid flowfield of a high speed inlet by the solution of the Euler equations. The lower-upper implicit scheme in conjunction with adaptive dissipation proves to be an efficient and robust nonoscillatory shock capturing technique for high Mach number flows as well as for transonic flows. |
| File Size | 586503 |
| Page Count | 18 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860014092 |
| Archival Resource Key | ark:/13960/t94798n1n |
| Language | English |
| Publisher Date | 1986-04-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Navier-stokes Equation Robustness Mathematics Shock Waves Transonic Flow Computational Fluid Dynamics Euler Equations of Motion Flow Distribution Finite Volume Method Inlet Flow Mach Number Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
