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Analytical studies of separated vortex flow on highly swept wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Kuhlman, J. M. |
| Copyright Year | 1978 |
| Description | A subsonic potential flow mathematical model of the flow past slender aerodynamic surfaces with sharp edges and separated vortex flow is reported. Comparisons with experimental data are presented for overall forces and pressure distributions for a series of thin, low aspect ratio wings, including both flat and conically cambered ones. A discussion is presented of the limitations of the current theory, and some suggestions are made as to how the theory might be improved. Details of program data input modifications for three-dimensional geometry are described in an appendix. |
| File Size | 1352220 |
| Page Count | 65 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19790004835 |
| Archival Resource Key | ark:/13960/t1kh5cw13 |
| Language | English |
| Publisher Date | 1978-11-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Slender Wings Low Aspect Ratio Wings Vortices Subsonic Flow Delta Wings Sharp Leading Edges Mathematical Models Angle of Attack Separated Flow Ntrs Nasa Technical Reports Server (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |
