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Test problems for inviscid transonic flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Carlson, L. A. |
| Copyright Year | 1979 |
| Description | Solving of test problems with the TRANDES program is discussed. This method utilizes the full, inviscid, perturbation potential flow equation in a Cartesian grid system that is stretched to infinity. This equation is represented by a nonconservative system of finite difference equations that includes at supersonic points a rotated difference scheme and is solved by column relaxation. The solution usually starts from a zero perturbation potential on a very coarse grid (typically 13 by 7) followed by several grid halvings until a final solution is obtained on a fine grid (97 by 49). |
| File Size | 4861447 |
| Page Count | 57 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790021971 |
| Archival Resource Key | ark:/13960/t4rj9826r |
| Language | English |
| Publisher Date | 1979-09-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Perturbation Theory Shock Waves Transonic Flow Fluid Dynamics Airfoil Profiles Finite Difference Theory Inviscid Flow Taylor Series Airfoils Computer Programs Cartesian Coordinates Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |
