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A supersonic, three-dimensional code for flow over blunt bodies: user's manual
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Chaussee, D. S. McMillan, O. J. |
| Copyright Year | 1980 |
| Description | A computer code is described which may be used to calculate the steady, supersonic, three-dimensional, inviscid flow over blunt bodies. The theoretical and numerical formulation of the problem is given (shock-capturing, downstream marching), including exposition of the boundary and initial conditions. The overall flow logic of the program, its usage, accuracy, and limitations are discussed. |
| File Size | 1630512 |
| Page Count | 28 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19800006790 |
| Archival Resource Key | ark:/13960/t1gj49d8d |
| Language | English |
| Publisher Date | 1980-01-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Supersonic Flow Three Dimensional Flow Computational Fluid Dynamics Finite Difference Theory Inviscid Flow Blunt Bodies User Manuals Computer Programs Boundary Layers Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
