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A computational system for aerodynamic design and analysis of supersonic aircraft. part 2: user's manual
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Coleman, R. G. Middleton, W. D. Lundry, J. L. |
| Copyright Year | 1976 |
| Description | An integrated system of computer programs was 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 user's manual contains a description of the system, an explanation of its usage, the input definition, and example output. |
| File Size | 10573515 |
| Page Count | 268 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19770004062 |
| Archival Resource Key | ark:/13960/t7np6vb4j |
| Language | English |
| Publisher Date | 1976-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Pressure Distribution Supersonic Aircraft Aerodynamic Configurations Cdc 6000 Series Computers User Manuals Computer Programs Fortran Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |