Loading...
Please wait, while we are loading the content...
Similar Documents
Development of a nonlinear vortex method. [steady and unsteady aerodynamic loads of highly sweptback wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kandil, O. A. |
| Copyright Year | 1981 |
| Description | Progress is reported in the development of reliable nonlinear vortex methods for predicting the steady and unsteady aerodynamic loads of highly sweptback wings at large angles of attack. Abstracts of the papers, talks, and theses produced through this research are included. The modified nonlinear discrete vortex method and the nonlinear hybrid vortex method are highlighted. |
| File Size | 1417169 |
| Page Count | 35 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810015489 |
| Archival Resource Key | ark:/13960/t2x39m78m |
| Language | English |
| Publisher Date | 1981-05-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Computational Fluid Dynamics Vortices Unsteady Aerodynamics Abstracts Pressure Distribution Nonlinearity Angle of Attack Prediction Analysis Techniques Sweptback Wings Aerodynamic Loads 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 |
