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Approximate method for calculating transonic flow about lifting wing-body configurations: computer program and user's manual
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Barnwell, R. W. Davis, R. M. |
| Copyright Year | 1975 |
| Description | A user's manual is presented for a computer program which calculates inviscid flow about lifting configurations in the free-stream Mach-number range from zero to low supersonic. Angles of attack of the order of the configuration thickness-length ratio and less can be calculated. An approximate formulation was used which accounts for shock waves, leading-edge separation and wind-tunnel wall effects. |
| File Size | 11158366 |
| Page Count | 137 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19750022026 |
| Archival Resource Key | ark:/13960/t7xm3381r |
| Language | English |
| Publisher Date | 1975-08-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Tables Data Computer Programming Shock Waves Transonic Flow Body-wing Configurations Lifting Bodies Wing Profiles Angle of Attack Leading Edges User Manuals Computer Programs Digital Data Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |