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Separation behavior of boundary layers on three-dimensional wings
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Stock, H. W. |
| Copyright Year | 1981 |
| Description | An inverse boundary layer procedure for calculating separated, turbulent boundary layers at infinitely long, crabbing wing was developed. The procedure was developed for calculating three dimensional, incompressible turbulent boundary layers was expanded to adiabatic, compressible flows. Example calculations with transsonic wings were made including viscose effects. In this case an approximated calculation method described for areas of separated, turbulent boundary layers, permitting calculation of this displacement thickness. The laminar boundary layer development was calculated with inclined ellipsoids. |
| File Size | 2324773 |
| Page Count | 76 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19810010501 |
| Archival Resource Key | ark:/13960/t0kt1hg9j |
| Language | English |
| Publisher Date | 1981-02-01 |
| Access Restriction | Open |
| Subject Keyword | Aerodynamics Turbulent Flow Three Dimensional Flow Airfoils Mathematical Models Velocity Distribution Separated Flow Boundary Layers Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |