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A computational system for aerodynamic design and analysis of 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 | 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. Schematics of the program structure and the individual overlays and subroutines are described. |
| File Size | 4739443 |
| Page Count | 84 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19760021073 |
| Archival Resource Key | ark:/13960/t6rz4227j |
| Language | English |
| Publisher Date | 1976-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Wings Supersonic Aircraft Wave Drag Computer Graphics Pressure Distribution Aircraft Design Aerodynamic Characteristics Aircraft Configurations 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 |