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Influence matrix program for aerodynamic lifting surface theory. [in subsonic flows
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Ray, K. S. Medan, R. T. |
| Copyright Year | 1973 |
| Description | A users manual is described for a USA FORTRAN 4 computer program which computes an aerodynamic influence matrix and is one of several computer programs used to analyze lifting, thin wings in steady, subsonic flow according to a kernel function method lifting surface theory. The most significant features of the program are that it can treat unsymmetrical wings, control points can be placed on the leading and/or trailing edges, and a stable, efficient algorithm is used to compute the influence matrix. |
| File Size | 1040431 |
| Page Count | 62 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19740008588 |
| Archival Resource Key | ark:/13960/t91882n2p |
| Language | English |
| Publisher Date | 1973-12-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Kernel Functions Lifting Bodies Subsonic Flow Trailing Edges Thin Wings User Manuals Computer Programs Fortran Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
