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Boundary condition computational procedures for inviscid, supersonic steady flow field calculations
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Abbett, M. J. |
| Copyright Year | 1971 |
| Description | Results are given of a comparative study of numerical procedures for computing solid wall boundary points in supersonic inviscid flow calculatons. Twenty five different calculation procedures were tested on two sample problems: a simple expansion wave and a simple compression (two-dimensional steady flow). A simple calculation procedure was developed. The merits and shortcomings of the various procedures are discussed, along with complications for three-dimensional and time-dependent flows. |
| File Size | 4443013 |
| Page Count | 93 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19720014686 |
| Archival Resource Key | ark:/13960/t0jt4ds6q |
| Language | English |
| Publisher Date | 1971-11-30 |
| Access Restriction | Open |
| Subject Keyword | Fluid Mechanics Inviscid Flow Boundary Conditions Numerical Analysis Fluid Boundaries Supersonic Speed Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
