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Airfoil profile in a nonuniform flow
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Polasek, J. |
| Copyright Year | 1978 |
| Description | A theory of airfoil section past two dimensional nonuniform flow is developed. The theory is based on representation of airfoil section by vortex and source distributions and it can be used for calculation of aircraft wings in homogeneous and inhomogeneous flow, as well as for calculation of straight and radial blade and vane-cascades. |
| File Size | 1780033 |
| Page Count | 53 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19780013105 |
| Archival Resource Key | ark:/13960/t4qk26z9d |
| Language | English |
| Publisher Date | 1978-03-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Nonuniform Flow Blade Tips Wings Airfoil Profiles Vortices Vanes Aircraft Parts Two Dimensional Flow Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Article |