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Aerodynamic design and analysis system for supersonic aircraft. part 1: general description and theoretical development
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Middleton, W. D. Lundry, J. L. |
| Copyright Year | 1975 |
| Description | An integrated system of computer programs has been developed for the design and analysis of supersonic configurations. The system uses linearized theory methods for the calculation of surface pressures and supersonic area rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients. Interactive graphics are optional at the user's request. This part presents a general description of the system and describes the theoretical methods used. |
| File Size | 2827470 |
| Page Count | 79 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750010113 |
| Archival Resource Key | ark:/13960/t1jh8b66z |
| Language | English |
| Publisher Date | 1975-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Numerical Analysis Aerodynamic Configurations Supersonic Speed Computer Techniques Data Processing Aerodynamic Coefficients Systems Analysis Aircraft Design Computer Aided Design Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
