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Input description for jameson's three-dimensional transonic airfoil analysis program
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Davis, R. M. Newman, P. A. |
| Copyright Year | 1974 |
| Description | The input parameters are presented for a computer program which performs calculations for inviscid isentropic transonic flow over three dimensional airfoils with straight leading edges. The free stream Mach number is restricted only by the isentropic assumption. Weak shock waves are automatically located where they occur in the flow. The finite difference form of the full equation for the velocity potential is solved by the method of relaxation, after the flow exterior to the airfoil is mapped to the upper half plane. |
| File Size | 754797 |
| Page Count | 29 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740011527 |
| Archival Resource Key | ark:/13960/t0101xx36 |
| Language | English |
| Publisher Date | 1974-02-07 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Air Flow Flow Equations Transonic Flow Numerical Analysis Aerodynamic Configurations Airfoil Profiles Finite Difference Theory Inviscid Flow 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 |
