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Estimation of wing nonlinear aerodynamic characteristics at supersonic speeds
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Mack, R. J. Carlson, H. W. |
| Copyright Year | 1980 |
| Description | A computational system for estimation of nonlinear aerodynamic characteristics of wings at supersonic speeds was developed and was incorporated in a computer program. This corrected linearized theory method accounts for nonlinearities in the variation of basic pressure loadings with local surface slopes, predicts the degree of attainment of theoretical leading edge thrust, and provides an estimate of detached leading edge vortex loadings that result when the theoretical thrust forces are not fully realized. |
| File Size | 2650689 |
| Page Count | 84 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810001496 |
| Archival Resource Key | ark:/13960/t7wm63c6b |
| Language | English |
| Publisher Date | 1980-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Dynamic Characteristics Leading Edge Thrust Supersonic Speed Variability Wind Tunnel Tests Nonlinearity Aerodynamic Characteristics Wing Loading Computer Programs Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |