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Aerodynamic design and analysis system for supersonic aircraft. part 3: computer program description
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Coleman, R. G. Middleton, W. D. Lundry, J. L. |
| Copyright Year | 1975 |
| Description | The computer program for the design and analysis of supersonic aircraft configurations is presented. The schematics of the program structure are provided. The individual overlays and subroutines are described. The system is useful in determining surface pressures and supersonic area rule concepts. |
| File Size | 3619613 |
| Page Count | 98 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750010114 |
| Archival Resource Key | ark:/13960/t08w8652z |
| Language | English |
| Publisher Date | 1975-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Subroutines Numerical Analysis Aerodynamic Configurations Supersonic Speed Computer Techniques Data Processing Systems Analysis Aircraft Design Computer Aided Design Computer Programs Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |