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Vortex lift research: early contributions and some current challenges
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Polhamus, E. C. |
| Copyright Year | 1986 |
| Description | The trend towards slender wing aircraft for supersonic cruise and the early chronology of research directed towards their vortex-lift characteristics are briefly reviewed. An overview of the development of vortex-lift theoretical methods is presented, and some current computational and experimental challenges related to the viscous flow aspects of this vortex flow are discussed. |
| File Size | 2592813 |
| Page Count | 30 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19860017719 |
| Archival Resource Key | ark:/13960/t03z34w38 |
| Language | English |
| Publisher Date | 1986-07-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Vortex Sheets Aircraft Stability Computational Fluid Dynamics Lift Drag Ratio Aircraft Design Lift Slender Wings Vortices Subsonic Flow Separated Flow Aircraft Configurations Fighter Aircraft Leading Edges Viscous Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |